diff --git a/data/pds4/Notes.txt b/data/pds4/Notes.txt new file mode 100644 index 00000000..86430bed --- /dev/null +++ b/data/pds4/Notes.txt @@ -0,0 +1,67 @@ +Notes from context clean-up activities +====================================== + +Missing values +------------------------------- + +Context: Product_Context/Reference_List/Internal_Reference + investigation_to_agency + investigation_to_investigation (for large observing campaigns with + separately organized groups working independently, and for + legacy extended missions that do not have multiple mission + names in the data or references). + +Context: Product_*/Identification_Area/Licensing/Internal_Reference + ??? The DPH description and implementation here is seriously problematic. + PDS should absolutely not be creating its own URI for licenses + that have public, well-supported URIs, or implying that it will + somehow be independently versioning these licenses. It also + separates any license and CC0 from its legal definition. This + DEFEATS usability. Also, CCO is NOT a license and the language + in the DPH repeatedly describing it as such is just flat-out + wrong. + + + +Questions +========= + +General +------- + o What should we do about "To Do" lists in the investigation context + objects? I'm finding these for legacy data that is not going to be + migrated any time soon, and resolving them ultimately requires + working up and down the reference chain. Are we expected to do that + now? Later? If not now, what is the point of carrying comments in + the context object as opposed to, say, an errata file or something + that might be visible to a user interested in the investigation? + + o 256 characters seems ridiculously short for a "description" field. + It's only one character longer than the "title" field. If the + intention is to enforce it, then it needs to be schematically + enforced or it will be ignored. I suggest it would be more useful + to describe how to write a description, and only display the + first 80-256 characters unless a user requests to see more. + +Telescopes +---------- + + o For portable telescopes, should there be a "facility" product + created to identify the owner of the portable telescope for + inclusion in the investigation reference list? + +Missions +-------- + + o Should extended missions link to all precursor missions or only + the immediate precursor? Should there be a special + for this? + + o Should primary missions link to all extended missions, or only + the immediate successor mission? Should there be a special + for this? + + o When one mission is designed specifically to observe the + aftermath of a completely separate mission, should these + mission context products reference each other? If so, should + there be a special for this case? diff --git a/data/pds4/context-pds4/investigation/Collection_investigation_v19.0.csv b/data/pds4/context-pds4/investigation/Collection_investigation_v19.0.csv new file mode 100644 index 00000000..c319ed57 --- /dev/null +++ b/data/pds4/context-pds4/investigation/Collection_investigation_v19.0.csv @@ -0,0 +1,186 @@ +P,urn:nasa:pds:context:investigation:field_campaign.dd_eldorado_nv_2015::1.0 +P,urn:nasa:pds:context:investigation:individual.campbell_venus_radar::1.0 +P,urn:nasa:pds:context:investigation:individual.carbonate_refractive_indices::1.0 +P,urn:nasa:pds:context:investigation:individual.catalina_sky_survey::1.0 +P,urn:nasa:pds:context:investigation:individual.catalina_sky_survey::2.0 +P,urn:nasa:pds:context:investigation:individual.frankenspectra::1.0 +P,urn:nasa:pds:context:investigation:individual.goldstone_raw_radar::1.0 +P,urn:nasa:pds:context:investigation:individual.greeley_35mm_slides::1.0 +P,urn:nasa:pds:context:investigation:individual.greeley_field_amboycrater::1.0 +P,urn:nasa:pds:context:investigation:individual.lab_shocked_feldspars::1.0 +P,urn:nasa:pds:context:investigation:individual.lab_shocked_feldspars::2.0 +P,urn:nasa:pds:context:investigation:individual.lowell_observatory_near_earth_object_survey::1.0 +P,urn:nasa:pds:context:investigation:individual.lowell_observatory_near_earth_object_survey::2.0 +P,urn:nasa:pds:context:investigation:individual.near_earth_asteroid_tracking::1.0 +P,urn:nasa:pds:context:investigation:individual.near_earth_asteroid_tracking::2.0 +P,urn:nasa:pds:context:investigation:individual.none::1.0 +P,urn:nasa:pds:context:investigation:individual.none::2.0 +P,urn:nasa:pds:context:investigation:individual.spacewatch::1.0 +P,urn:nasa:pds:context:investigation:individual.spacewatch::2.0 +P,urn:nasa:pds:context:investigation:individual.titan-material-database::1.0 +P,urn:nasa:pds:context:investigation:individual.xas_synthesized_glasses::1.0 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urn:nasa:pds:context:investigation:* context products + 1.20.0.0 + Product_Collection + + PDS Data Design Working Group (DDWG) + PDS Change Control Board (CCB) + 2024 + The PDS4 Context Products for Investigations, e.g. Mars2020 mission, IRTF observing campaign + + + + 2024-08-01 + 19.0 + +added: + P,urn:nasa:pds:context:investigation:individual.catalina_sky_survey::2.0 + P,urn:nasa:pds:context:investigation:individual.lowell_observatory_near_earth_object_survey::2.0 + P,urn:nasa:pds:context:investigation:individual.near_earth_asteroid_tracking::2.0 + P,urn:nasa:pds:context:investigation:individual.none::2.0 + P,urn:nasa:pds:context:investigation:individual.spacewatch::2.0 + P,urn:nasa:pds:context:investigation:mission.bopps::2.0 + P,urn:nasa:pds:context:investigation:mission.contour_mission::2.0 + P,urn:nasa:pds:context:investigation:mission.dawn_mission_to_vesta_and_ceres::2.0 + P,urn:nasa:pds:context:investigation:mission.deep_impact::2.0 + P,urn:nasa:pds:context:investigation:mission.deep_space_1::2.0 + + + + 2024-06-09 + 18.0 + +added: + P,urn:nasa:pds:context:investigation:individual.frankenspectra::1.0 + + + 2024-05-13 + 17.0 + +added: + P,urn:nasa:pds:context:investigation:mission.clps_to_2ab::1.0 + P,urn:nasa:pds:context:investigation:mission.new_horizons::2.0 + P,urn:nasa:pds:context:investigation:mission.new_horizons_kem1::1.1 + P,urn:nasa:pds:context:investigation:other_investigation.clps::1.0 + + + 2024-02-12 + 16.0 + +added: + P,urn:nasa:pds:context:investigation:individual.lowell_observatory_near_earth_object_survey::1.0 + P,urn:nasa:pds:context:investigation:individual.titan-material-database::1.0 + P,urn:nasa:pds:context:investigation:mission.pioneer_venus::2.0 + + + 2023-09-17 + 15.0 + +added: + P,urn:nasa:pds:context:investigation:mission.ladee::1.3 + + + 2023-06-20 + 14.0 + +added: + P,urn:nasa:pds:context:investigation:mission.clipper::1.0 + P,urn:nasa:pds:context:investigation:mission.near_earth_asteroid_rendezvous::1.2 + + + 2023-02-01 + 13.0 + +added: + P,urn:nasa:pds:context:investigation:mission.new_horizons_kem1::1.0 + + + 2022-11-10 + 12.0 + +added: + P,urn:nasa:pds:context:investigation:individual.goldstone_raw_radar::1.0 + P,urn:nasa:pds:context:investigation:mission.infrared_astronomical_satellite::2.0 + + + 2022-08-23 + 11.0 + +added: + P,urn:nasa:pds:context:investigation:mission.hayabusa::2.0 + + + 2022-06-25 + 10.0 + +added: + P,urn:nasa:pds:context:investigation:mission.neas::1.0 + P,urn:nasa:pds:context:investigation:mission.psyche::1.0 + + + 2022-05-31 + 9.0 + +added: + P,urn:nasa:pds:context:investigation:mission.lunar_trailblazer::1.0 + + + 2022-03-03 + 8.0 + +added: + P,urn:nasa:pds:context:investigation:individual.xas_synthesized_glasses::1.0 + + + 2021-12-08 + 7.0 + +added: + P,urn:nasa:pds:context:investigation:individual.near_earth_asteroid_tracking::1.0 + P,urn:nasa:pds:context:investigation:mission.apollo_11::1.0 + P,urn:nasa:pds:context:investigation:mission.double_asteroid_redirection_test::1.0 + P,urn:nasa:pds:context:investigation:mission.light_italian_cubesat_for_imaging_of_asteroids::1.0 + P,urn:nasa:pds:context:investigation:observing_campaign.earth-based-uranus-stellar-occultations::1.0 + P,urn:nasa:pds:context:investigation:observing_campaign.irtf_io::1.1 + P,urn:nasa:pds:context:investigation:observing_campaign.jupiter_support::1.1 + P,urn:nasa:pds:context:investigation:other_investigation.astromat_data::1.0 + + + 2021-09-16 + 6.0 + +added: + P,urn:nasa:pds:context:investigation:individual.campbell_venus_radar::1.0 + + + 2021-06-21 + 5.0 + +added: + P,urn:nasa:pds:context:investigation:individual.greeley_35mm_slides::1.0 + + + 2021-05-13 + 4.0 + +added: + P,urn:nasa:pds:context:investigation:mission.neowise::1.0 + P,urn:nasa:pds:context:investigation:mission.wise::1.0 + + + 2021-03-18 + 3.0 + +added: + P,urn:nasa:pds:context:investigation:individual.catalina_sky_survey::1.0 + P,urn:nasa:pds:context:investigation:individual.spacewatch::1.0 + + + 2021-03-02 + 2.0 + +added: + P,urn:nasa:pds:context:investigation:field_campaign.dd_eldorado_nv_2015::1.0 + P,urn:nasa:pds:context:investigation:mission.cassini-huygens::1.2 + P,urn:nasa:pds:context:investigation:mission.cassini-huygens::1.3 + P,urn:nasa:pds:context:investigation:mission.comet_sl9-jupiter_collision::1.2 + P,urn:nasa:pds:context:investigation:mission.mars2020::1.0 + + + 2021-01-13 + 1.0 + This is the initial version of the Collection product. + + + + + + urn:nasa:pds:context + collection_to_bundle + + + + Context + + + + Collection_investigation_v18.0.csv + 2024-06-09T07:36:37Z + 12091 + 176 + f557b12bebc65cd6464b1c2d25dc7247 + + + 0 + PDS DSV 1 + 186 + Carriage-Return Line-Feed + Comma + + 2 + 0 + 102 + + Member Status + 1 + ASCII_String + 1 + %1s + Member Status of the files in the collection. + + + LIDVID_LID + 2 + ASCII_LIDVID_LID + 255 + %-255s + LIDVIDs of the files. + + + inventory_has_member_product + + + diff --git a/data/pds4/context-pds4/investigation/individual.catalina_sky_survey_2.0.xml b/data/pds4/context-pds4/investigation/individual.catalina_sky_survey_2.0.xml new file mode 100644 index 00000000..72d041b4 --- /dev/null +++ b/data/pds4/context-pds4/investigation/individual.catalina_sky_survey_2.0.xml @@ -0,0 +1,71 @@ + + + + + + urn:nasa:pds:context:investigation:individual.catalina_sky_survey + 2.0 + Catalina Sky Survey + 1.22.0.0 + Product_Context + + + CSS + + + + + 2024-07-31 + 2.0 + + Edited to comply with Editorial Working Group checklist. + + + + 2021-03-10 + 1.0 + Initial version + + + + + + urn:nasa:pds:context:agency:agency.nasa + context_to_associate + investigation_to_agency + + + urn:nasa:pds:context:facility:observatory.mount_bigelow + investigation_to_facility + + + urn:nasa:pds:context:facility:observatory.mount_lemmon + investigation_to_facility + + + urn:nasa:pds:context:facility:observatory.siding_spring + investigation_to_facility + + + urn:nasa:pds:context:facility:observatory.steward-kittpeak + investigation_to_facility + + + urn:nasa:pds:context_support:document:css_description + investigation_to_document + Description of the Catalina Sky Survey + + + + Catalina Sky Survey + Individual Investigation + 1998 + + + The Catalina Sky Survey (CSS) is a NASA funded project fully dedicated to the discovery and tracking of near-Earth + objects (NEOs). + + + diff --git a/data/pds4/context-pds4/investigation/individual.lowell_observatory_near_earth_object_survey_2.0.xml b/data/pds4/context-pds4/investigation/individual.lowell_observatory_near_earth_object_survey_2.0.xml new file mode 100644 index 00000000..7d12bc18 --- /dev/null +++ b/data/pds4/context-pds4/investigation/individual.lowell_observatory_near_earth_object_survey_2.0.xml @@ -0,0 +1,58 @@ + + + + + + urn:nasa:pds:context:investigation:individual.lowell_observatory_near_earth_object_survey + 2.0 + Lowell Observatory Near-Earth Object Survey + 1.22.0.0 + Product_Context + + + LONEOS + + + + + 2024-07-31 + 2.0 + + Edited to comply with Editorial Working Group checklist. + + + + 2024-01-17 + 1.0 + Initial version + + + + + + urn:nasa:pds:context:agency:agency.nasa + context_to_associate + investigation_to_agency + + + urn:nasa:pds:context:facility:observatory.lowell + investigation_to_facility + + + urn:nasa:pds:context_support:document:loneos_description + investigation_to_document + + + + Individual Investigation + 1998 + 2008 + + The LONEOS was a 10-year, ground-based program at Lowell Observatory to search for + Near Earth Objects. It consisted of two parts, LONEOS-1 spanning 1998-2000, and + LONEOS-2, conducted with a more sensitive camera, spanning 2000-2008. + + + diff --git a/data/pds4/context-pds4/investigation/individual.near_earth_asteroid_tracking_2.0.xml b/data/pds4/context-pds4/investigation/individual.near_earth_asteroid_tracking_2.0.xml new file mode 100644 index 00000000..c5e4c4ec --- /dev/null +++ b/data/pds4/context-pds4/investigation/individual.near_earth_asteroid_tracking_2.0.xml @@ -0,0 +1,63 @@ + + + + + + urn:nasa:pds:context:investigation:individual.near_earth_asteroid_tracking + 2.0 + Near-Earth Asteroid Tracking + 1.22.0.0 + Product_Context + + + NEAT + + + + + 2024-07-31 + 2.0 + + Edited to comply with Editorial Working Group checklist. + + + + 2021-10-15 + 1.0 + Initial version + + + + + + urn:nasa:pds:context:agency:agency.nasa + context_to_associate + investigation_to_agency + + + urn:nasa:pds:context:facility:observatory.palomar + investigation_to_facility + + + urn:nasa:pds:context:facility:observatory.amos + investigation_to_facility + + + urn:nasa:pds:context_support:document:neat_description + investigation_to_document + + + + Near-Earth Asteroid Tracking + Individual Investigation + 1996-04-17 + 2007-04-15 + + The NEAT survey discovered and tracked near-Earth asteroids and comets + using telescopes in Hawai'i and at Palomar Observatory over the period + December 1995 - April 2007. + + + diff --git a/data/pds4/context-pds4/investigation/individual.none_2.0.xml b/data/pds4/context-pds4/investigation/individual.none_2.0.xml new file mode 100644 index 00000000..00c2d899 --- /dev/null +++ b/data/pds4/context-pds4/investigation/individual.none_2.0.xml @@ -0,0 +1,56 @@ + + + + + + + urn:nasa:pds:context:investigation:individual.none + 2.0 + No Specific Investigation + 1.22.0.0 + Product_Context + + + None + + + None Applicable + + + + + 2024-07-31 + 2.0 + + Edited to comply with Editorial Working Group checklist. + + + + 2018-06-14 + 1.0 + initial + + + + + + + urn:nasa:pds:context_support:document:none_description + investigation_to_document + + + + + No Specific Investigation + Individual Investigation + -9999-01-01 + + + This context object indicates there is no specific funded investigation + associated with the product. + + + diff --git a/data/pds4/context-pds4/investigation/individual.spacewatch_2.0.xml b/data/pds4/context-pds4/investigation/individual.spacewatch_2.0.xml new file mode 100644 index 00000000..325e7b6d --- /dev/null +++ b/data/pds4/context-pds4/investigation/individual.spacewatch_2.0.xml @@ -0,0 +1,48 @@ + + + + + + urn:nasa:pds:context:investigation:individual.spacewatch + 2.0 + Spacewatch + 1.22.0.0 + Product_Context + + + 2024-07-31 + 2.0 + + Edited to comply with Editorial Working Group checklist. + + + + 2021-03-10 + 1.0 + Initial version + + + + + + urn:nasa:pds:context:facility:observatory.steward-kittpeak + investigation_to_facility + + + urn:nasa:pds:context_support:document:spacewatch_dscription + investigation_to_document + + + + Individual Investigation + 1980 + + + SPACEWATCH® is a research group created to explore the various populations of small + objects in the solar system and study the statistics of asteroids and comets in order + to investigate the dynamical evolution of the solar system. + + + diff --git a/data/pds4/context-pds4/investigation/mission.bopps_2.0.xml b/data/pds4/context-pds4/investigation/mission.bopps_2.0.xml new file mode 100644 index 00000000..c60c5cd6 --- /dev/null +++ b/data/pds4/context-pds4/investigation/mission.bopps_2.0.xml @@ -0,0 +1,62 @@ + + + + + + + urn:nasa:pds:context:investigation:mission.bopps + 2.0 + Balloon Observation Platform for Planetary Science + 1.22.0.0 + Product_Context + + + BOPPS + + + Balloon Observation Platform for Planetary Science (BOPPS) - 2014 Flight + + + + + + 2024-07-31 + 2.0 + + Edited to comply with Editorial Working Group checklist. + + + + 2017-02-27 + 1.0 + + A.Raugh: Creation + + + + + + + + urn:nasa:pds:bopps2014:document:mission_overview + investigation_to_document + + This brief text document provides an overview of the BOPPS 2014 mission. + + + + + + Balloon Observation Platform for Planetary Science + Mission + 2014-09-25 + 2014-09-26 + + The 2014 BOPPS flight launched from Ft. Sumner, New Mexico at 8L20, and achieved and + altitude of 130,000 feet, from which it observed the asteroid (1) Ceres and comets + C/2013 A1 (Siding Spring) and C/2014 E2 (Jacques). + + + \ No newline at end of file diff --git a/data/pds4/context-pds4/investigation/mission.contour_mission_2.0.xml b/data/pds4/context-pds4/investigation/mission.contour_mission_2.0.xml new file mode 100644 index 00000000..f4366248 --- /dev/null +++ b/data/pds4/context-pds4/investigation/mission.contour_mission_2.0.xml @@ -0,0 +1,70 @@ + + + + + + + urn:nasa:pds:context:investigation:mission.contour_mission + 2.0 + Comet Nucleus Tour + 1.22.0.0 + Product_Context + + + CONTOUR + + + + + 2024-07-31 + 2.0 + + Edited to comply with Editorial Working Group checklist. + Also: + Replaced LIDVID spacecraft reference with LID + Removed External_Reference to nothing + Corrected title + + + + + 2016-10-01 + 1.0 + + extracted metadata from PDS3 catalog and + modified to comply with PDS4 Information Model + + + + + + + + urn:nasa:pds:context:agency:agency.nasa + context_to_associate + investigation_to_agency + + + urn:nasa:pds:context:instrument_host:spacecraft.con + investigation_to_instrument_host + + + urn:nasa:pds:context_support:description:contour_description + investigation_to_document + + + + + Comet Nucleus Tour + Mission + 2002-07-05 + 2002-08-15 + + + The Comet Nucleus Tour mission failed when the spacecraft broke + apart during a planned maneuver six weeks after launch. It + + + diff --git a/data/pds4/context-pds4/investigation/mission.dawn_mission_to_vesta_and_ceres_2.0.xml b/data/pds4/context-pds4/investigation/mission.dawn_mission_to_vesta_and_ceres_2.0.xml new file mode 100644 index 00000000..4ef73496 --- /dev/null +++ b/data/pds4/context-pds4/investigation/mission.dawn_mission_to_vesta_and_ceres_2.0.xml @@ -0,0 +1,155 @@ + + + + + + + urn:nasa:pds:context:investigation:mission.dawn_mission_to_vesta_and_ceres + 2.0 + Dawn + 1.22.0.0 + Product_Context + + + Dawn Mission to Vesta and Ceres + + + + + 2024-08-01 + 2.0 + + Edited to comply with Editorial Working Group checklist. + + + + 2019-01-03 + 1.1 + + Per "Guide toPDS4 Context Products" v1.3, + - changed all lidvid_reference to lid_reference + - changed target LIDs to new formation rule + + + + 2016-10-01 + 1.0 + + extracted metadata from PDS3 catalog and + modified to comply with PDS4 Information Model + + + + + + + + urn:nasa:pds:context:agency:agency.nasa + context_to_associate + investigation_to_agency + + + urn:nasa:pds:context:instrument_host:spacecraft.dawn + investigation_to_instrument_host + + + urn:nasa:pds:context:target:dwarf_planet.1_ceres + investigation_to_target + + + urn:nasa:pds:context:target:asteroid.4_vesta + investigation_to_target + + + urn:nasa:pds:context:target:planet.mars + investigation_to_target + + + urn:nasa:pds:context_support:document:dawn_description + investigation_to_document + + + urn:nasa:pds:context_support:image:dawn_mission_logo + investigation_to_document + + + 10.1007/s11214-011-9792-x + + Coradini, A., D. Turrini, C. Federico, and G. Magni, Vesta and Ceres: crossing + the history of the Solar system. Space Sci. Rev., + doi:10.1007/s11214-011-9792-x, 2011. + + + + 10.1007/s11214-010-9668-5 + + De Sanctis, M. C., A. Coradini, E. Ammannito, G. Filacchione, M.T. Capria, S. + Fonte, G. Magni, A. Barbis, A. Bini, M. Dami, I. Ficai-Veltroni, and G. Preti, + VIR Team, The VIR Spectrometer, Space Sci Rev, doi:10.1007/s11214-010-9668-5, + 2010. + + + + 10.1109/TNS.2003.815156 + + Prettyman, T.H., W.C. Feldman, F.P. Ameduri, B.L. Barraclough, E.W. Cascio, + K.R. Fuller, H.O. Funsten, D.J. Lawrence, G.W. McKinney, C.T. Russell, S.A. + Soldner, S.A. Storms, C. Szeles, and R.L. Tokar, Gamma-ray and neutron + spectrometer for the Dawn mission to 1 Ceres and 4 Vesta, IEEE Trans. Nucl. + Sci., Volume 50, Issue 4, pp. 1190-1197, August 2003, + doi:10.1109/TNS.2003.815156 + + + + 10.1007/s11214-011-9862-0 + + Prettyman, T.H., W.C. Feldman, H.Y. McSween, Jr., R.D. Dingler, D.C. Enemark, + D.E. Patrick, S.A. Storms, J.S. Hendricks, J.P. Morgenthaler, K.M. Pitman, R.C. + Reedy, Dawn's Gamma Ray and Neutron Detector, Space Sci. Rev. (2011) + 163:371-459, doi:10.1007/s11214-011-9862-0 + + + + 10.1016/j.actaastro.2006.01.014 + + Rayman, M.D., T.C. Fraschetti, C.A. Raymond, and C.T. Russell, Dawn: A mission + in development for exploration of main belt asteroids Vesta and Ceres, Acta + Astronautica 58, 605-616, 2006. + + + + + Raymond, C.A., Dawn Science Plan, JPL D-31827, 2007. + + + Note that this document is included in the PDS3 archive still waiting to + be migrated (by PPI node). + + + + + Schroeder, S.E., and P. Gutierrez-Marques, Calibration Pipeline, MPS Report + DA-FC-MPAE-RP-272, Issue 2, Rev. a, 20 July 2011. + + + Note that this document is included in the PDS3 archive still waiting to + be migrated (by PPI node). + + + + + + Dawn + Mission + 2007-09-27 + 2016-07-01 + + + The Dawn mission visited the dwarf planet Ceres and asteroid Vesta. Dawn launched + in September 2007. Communication with the spacecraft was lost after hydrazine + exhaustion in October 2018. + + + diff --git a/data/pds4/context-pds4/investigation/mission.deep_impact_2.0.xml b/data/pds4/context-pds4/investigation/mission.deep_impact_2.0.xml new file mode 100644 index 00000000..d2d6c3b0 --- /dev/null +++ b/data/pds4/context-pds4/investigation/mission.deep_impact_2.0.xml @@ -0,0 +1,364 @@ + + + + + + + urn:nasa:pds:context:investigation:mission.deep_impact + 2.0 + Deep Impact + 1.22.0.0 + Product_Context + + + DI + DI + + + + + 2024-08-01 + 2.0 + + Edited to comply with Editorial Working Group checklist. + + + + 2019-01-03 + 1.1 + + Per "Guide toPDS4 Context Products" v1.3, + - changed all lidvid_reference to lid_reference + - changed target LIDs to new formation rule + + + + 2016-10-01 + 1.0 + + extracted metadata from PDS3 catalog and + modified to comply with PDS4 Information Model + + + + + + + + + + + + + + + + urn:nasa:pds:context:agency:agency.nasa + context_to_associate + investigation_to_agency + + + urn:nasa:pds:context:instrument_host:spacecraft.dif + investigation_to_instrument_host + + + urn:nasa:pds:context:instrument_host:spacecraft.dii + investigation_to_instrument_host + + + urn:nasa:pds:context:target:calibrator.calibration + investigation_to_target + + + urn:nasa:pds:context:target:comet.9p_tempel_1 + investigation_to_target + + + urn:nasa:pds:context_support:docuent:di_description + investigation_to_document + + + 10.1016/j.icarus.2006.12.011 + + A'Hearn, M.F., and M.R. Combi, Deep Impact at Comet Tempel 1, Icarus, 187(1), + pp. 1-3, 2007, doi:10.1016/j.icarus.2006.12.011. + + + + 10.1126/science.1118923 + + A'Hearn, M.F., M.J.S. Belton, W.A. Delamere, J. Kissel, K.P. Klaasen, L.A. + McFadden, K.J. Meech, H.J. Melosh, P.H. Schultz, J.M. Sunshine, P.C. Thomas, J. + Veverka, D.K. Yeomans, M.W. Baca, I. Busko, C.J. Crockett, S.M. Collins, M. + Desnoyer, C.A. Eberhardy, C.M. Ernst, T.L. Farnham, L. Feaga, O. Groussin, D. + Hampton, S.I. Ipatov, J.-Y. Li, D. Lindler, C.M. Lisse, N. Mastrodemos, W.M. + Owen, J.E. Richardson, D.D. Wellnitz, and R.L. White, Deep Impact: Excavating + Comet Tempel 1, Science, 310, 258-264, 2005, doi:10.1126/science.1118923. + + + + 10.1007/s11214-005-3387-3 + + A'Hearn, M.F., M.J.S. Belton, A. Delamere, and W.H. Blume, Deep Impact: A + Large-Scale Active Experiment on a Cometary Nucleus, Space Science Reviews, + 117, 1-21, 2005, doi:10.1007/s11214-005-3387-3. + + + + 10.1007/s11214-005-3389-1 + + Belton, M.J.S., K.J. Meech, M.F. A'Hearn, O. Groussin, L. McFadden, C. Lisse, + Y.R. Fernandez, J. Pittachova, H. Hsieh, J. Kissel, K. Klaasen, P. Lamy, D. + Prialnik, J. Sunshine, and I. Toth, Deep Impact: Working Properties for the + Target Nucleus Comet 9P/Tempel 1, Space Science Reviews, 117, 137-160, 2005, + doi:10.1007/s11214-005-3389-1. + + + + 10.1016/j.icarus.2006.09.005 + + Belton, M.J.S, P. Thomas, J. Veverka, P. Schultz, M.F. A'Hearn, L. Feaga, T. + Farnham, O. Groussin, J.-Y. Li, C. Lisse, L. McFadden, J. Sunshine, K.J. Meech, + W.A. Delamere, and J. Kissel, The internal structure of Jupiter family cometary + nuclei from Deep Impact observations: The 'talps' or 'layered pile' model, + Icarus, 187, 332-344, 2007, doi:10.1016/j.icarus.2006.09.005. + + + + 10.1007/s11214-005-3386-4 + + Blume, W.H., Deep Impact Mission Design, Space Science Reviews, 117, 23-42, + 2005, doi:10.1007/s11214-005-3386-4. + + + + 10.1016/j.icarus.2006.11.012 + + Busko, I., D. Lindler, M.F. A'Hearn, and R.L. White, Searching for the Deep + Impact crater on Comet 9P/Tempel 1 using image processing techniques, Icarus, + 187, 56-68, 2007, doi:10.1016/j.icarus.2006.11.012. + + + + + Ernst, C.M., and P.H. Schultz, Temporal and Spatial Resolution of the + Early-Time Impact Flash: Implications for Light Source Distribution, 38th Lunar + and Planetary Science Conference, LPI Contribution No. 1338, p. 2353, 2007. + + + + 10.1016/j.icarus.2006.10.036 + + Farnham, T.L., D.D. Wellnitz, D.L. Hampton, J.-Y. Li, J.M. Sunshine, O. + Groussin, L.A. McFadden, C.J. Crockett, M.F. A'Hearn, M.J.S. Belton, P. + Schultz, and C.M. Lisse, Dust coma morphology in the Deep Impact images of + Comet 9P/Tempel 1, Icarus, 187, 26-40, 2007, doi:10.1016/j.icarus.2006.10.036. + + + + 10.1016/j.icarus.2007.04.009 + + Feaga, L.M., M.F. A'Hearn, J.M. Sunshine, O. Groussin, and T.L. Farnham, + Asymmetries in the distribution of H2O and CO2 in the inner coma of Comet + 9P/Tempel 1 as observed by Deep Impact, Icarus, 190, 345-356, 2007, + doi:10.1016/j.icarus.2007.04.009. + + + + 10.1016/j.icarus.2006.08.030 + + Groussin, O., M.F. A'Hearn, J.-Y. Li, P.C. Thomas, J.M. Sunshine, C.M. Lisse, + K.J. Meech, T.L. Farnham, L.M. Feaga, and W.A. Delamere, Surface temperature of + the nucleus of Comet 9P/Tempel 1, Icarus, 187, 16-25, 2007, + doi:10.1016/j.icarus.2006.08.030. + + + + 10.1007/s11214-005-3390-8 + + Hampton, D.L., J.W. Baer, M.A. Huisjen, C.C. Varner, A. Delamere, D.D. + Wellnitz, M.F. A'Hearn, and K.P. Klaasen, An Overview of the Instrument Suite + for the Deep Impact Mission, Space Science Reviews, 117, 43-93, 2005, + doi:10.1007/s11214-005-3390-8. + + + + 10.1007/s11214-005-3385-5 + + Klaasen, K.P., B. Carcich, G. Carcich, E.J. Grayzeck, and S. McLaughlin, Deep + Impact: The Anticipated Flight Data, Space Science Reviews, 117, 335-372, 2005, + doi:10.1007/s11214-005-3385-5. + + + + 10.1063/1.2972112 + + Klaasen, K.P., M.F. A'Hearn, M. Baca, A. Delamere, M. Desnoyer, T. Farnham, O. + Groussin, D. Hampton, S. Ipatov, J. Li, C. Lisse, N. Mastrodemos, S. + McLaughlin, J. Sunshine, P. Thomas, and D. Wellnitz, Deep Impact Instrument + Calibration, Rev. Sci. Instrum., 79, 091301, 2008, doi:10.1063/1.2972112. + + + + 10.1016/j.icarus.2006.09.018 + + Li, J.-Y., M.F. A'Hearn, M.J.S. Belton, C.J. Crockett, T.L. Farnham, C.M. + Lisse, L.A. McFadden, K.J. Meech, J.M. Sunshine, P.C. Thomas, and J. Veverka, + Deep Impact photometry of Comet 9P/Tempel 1, Icarus, 187, 41-55, 2007, + doi:10.1016/j.icarus.2006.09.018. + + + + 10.1086/516829 + + Lindler, D., I. Busko, M.F. A'Hearn, and R.L. White, Restoration of Images of + Comet 9P/Tempel 1 Taken with the Deep Impact High Resolution Instrument, PASP, + 119, 427-436, 2007, doi:10.1086/516829. + + + + 10.1007/s11214-005-3384-6 + + Lisse, C.M., M.F. A'Hearn, T.L. Farnham, O. Groussin, K.J. Meech, U. Fink, and + D.G. Schleicher, The Coma of Comet 9P/Tempel 1, Space Science Reviews, 117, + 161-192, 2005, doi:10.1007/s11214-005-3384-6. + + + + 10.1007/s11214-005-3394-4 + + Mastrodemos, N., D.G. Kubitschek, and S.P. Synnott, Autonomous Navigation for + the Deep Impact Mission Encounter with with Comet Tempel 1. Space Science + Reviews, 117, 95-121, 2005, doi:10.1007/s11214-005-3394-4. + + + + 10.1007/s11214-005-6062-9 + + McFadden, L.A., M.K. Rountree-Brown, E.M. Warner, S.A. McLaughlin, J.M. Behne, + J.D. Ristvey, S. Baird-Wilkerson, D.K. Duncan, S.D. Gillam, G.H Walker, and + K.J. Meech, Education and Public Outreach for NASA's Deep Impact Mission, Space + Science Reviews, 117, 373-396, 2005, doi:10.1007/s11214-005-6062-9. + + + + 10.1007/s11214-005-3382-8 + + Meech, K.J., M.F. A'Hearn, Y.R. Fernandez, C.M. Lisse, H.A. Weaver, N. Biver, + and L.M. Woodney, The Deep Impact Earth-Based Campaign, Space Science Reviews, + 117, 297-334, 2005, doi:10.1007/s11214-005-3382-8. + + + + + Richardson, J.E., and H.J. Melosh, Modeling the Ballistic Behavior of Solid + Ejecta from the Deep Impact Cratering Event, 37th Annual Lunar and Planetary + Science Conference, Abstract no. 1836, 2006. + + + + + Richardson, J.E., Improving the Modeling of Impact Ejecta Behavior: The Effects + of Gravity and Strength near the Crater Rim, 38th Lunar and Planetary Science + Conference, LPI Contribution No. 1338, p. 1345, 2007. + + + + 10.1007/s11214-005-3393-5 + + Richardson, J.E., H.J. Melosh, N.A. Artemeiva, and E. Pierazzo, Impact + Cratering Theory and Modeling for the Deep Impact Mission: From Mission + Planning to Data Analysis, Space Science Reviews, 117, 241-267, 2005, + doi:10.1007/s11214-005-3393-5. + + + + 10.1007/s11214-005-3383-7 + + Schultz, P.H., C.M. Ernst, and J.L.B. Anderson, Expectations for Crater Size + and Photometric Evolution from the Deep Impact Collision, Space Science + Reviews, 117, 207-239, 2005, doi:10.1007/s11214-005-3383-7. + + + + + Schultz, P.H., Eberhardy, C.A., and C.M. Ernst, Initial Stages of the Deep + Impact Collision, 38th Lunar and Planetary Science Conference, LPI Contribution + No. 1338, p. 1890, 2007. + + + + 10.1007/s11214-005-3388-2 + + Sunshine, J.M., M.F. A'Hearn, O. Groussin, L. McFadden, K.P. Klaasen, P.H. + Schultz, and C.M. Lisse, Expectations for Infrared Spectroscopy of 9P/Tempel 1 + from Deep Impact, Space Science Reviews, 117, 269-295, 2005, + doi:10.1007/s11214-005-3388-2. + + + + 10.1126/science.1123632 + + Sunshine, J.M., M.F. A'Hearn, O. Groussin, J.-Y. Li, M.J.S. Belton, W.A. + Delamere, J. Kissel, K.P. Klaasen, L.A. McFadden, K.J. Meech, H.J. Melosh, P.H. + Schultz, P.C. Thomas, J. Veverka, D.K. Yeomans, I.C. Busko, M. Desnoyer, T.L. + Farnham, L.M. Feaga, D.L. Hampton, D.J. Lindler, C.M. Lisse, and D.D. Wellnitz, + Exposed Water Ice Deposits on the Surface of Comet 9P/Tempel 1, Science, 311, + 1453-1455, 2006, doi:10.1126/science.1123632. + + + + 10.1016/j.icarus.2007.04.024 + + Sunshine, J.M., O. Groussin, P.H. Schultz, M.F. A'Hearn, L.M. Feaga, T.L. + Farnham, and K.P. Klaasen, The distribution of water ice in the interior of + Comet Tempel 1, Icarus, Volume 190, 284-294, 2007, + doi:10.1016/j.icarus.2007.04.024. + + + + 10.1007/s11214-005-3391-7 + + Thomas, P.C., J. Veverka, M.F. A'Hearn, L. McFadden, M.J.S. Belton and J.M. + Sunshine, Comet Geology with Deep Impact Remote Sensing, Space Science Reviews, + 117, 193-205, 2005, doi:10.1007/s11214-005-3391-7. + + + + 10.1016/j.icarus.2006.12.013 + + Thomas, P.C, J. Veverka, M.J.S. Belton, A. Hidy, M.F. A'Hearn, T.L. Farnham, O. + Groussin, J.-Y. Li, L. A. McFadden, J. Sunshine, D. Wellnitz, C. Lisse, P. + Schultz, K. J. Meech, and W.A. Delamere, The shape, topography, and geology of + Tempel 1 from Deep Impact observations, Icarus, 187, 4-15, 2007, + doi:10.1016/j.icarus.2006.12.013. + + + + 10.1007/s11214-005-3392-6 + + Yeomans, D.K., J.D. Giorgini, and S.R. Chesley, The History and Dynamics of + Comet 9P/Tempel 1, Space Science Reviews, 117, 123-135, 2005, + doi:10.1007/s11214-005-3392-6. + + + + + + Deep Impact + Mission + 2005-01-12 + 2005-07-13 + + + The Deep Impact mission consisted of an impactor and a fly-by spacecraft that + rendezvoused with comet 9P/Tempel 1. The impactor was released to impact the + comet surface, while the flyby spacecraft observed. + + + diff --git a/data/pds4/context-pds4/investigation/mission.deep_space_1_2.0.xml b/data/pds4/context-pds4/investigation/mission.deep_space_1_2.0.xml new file mode 100644 index 00000000..d2eb2b8d --- /dev/null +++ b/data/pds4/context-pds4/investigation/mission.deep_space_1_2.0.xml @@ -0,0 +1,85 @@ + + + + + + + urn:nasa:pds:context:investigation:mission.deep_space_1 + 2.0 + Deep Space 1 + 1.22.0.0 + Product_Context + + + DS1 + + + + + 2024-08-01 + 2.0 + + Edited to comply with Editorial Working Group checklist. + + + + 2019-01-03 + 1.1 + + Per "Guide toPDS4 Context Products" v1.3, + - changed all lidvid_reference to lid_reference + - changed target LIDs to new formation rule + + + + 2016-10-01 + 1.0 + + extracted metadata from PDS3 catalog and + modified to comply with PDS4 Information Model + + + + + + + + urn:nasa:pds:context:agency:agency.nasa + context_to_associate + investigation_to_agency + + + urn:nasa:pds:context:instrument_host:spacecraft.ds1 + investigation_to_instrument_host + + + urn:nasa:pds:context:target:comet.19p_borrelly + investigation_to_target + + + urn:nasa:pds:context_support:document:ds1_description + investigation_to_document + + + + Rayman, M.D., The Successful Conclusion of the Deep Space 1 Mission: Important + Results without a Flashy Title, 53rd International Astronautical Congress/World + Space Congress, Houston, TX, IAC-02-Q.5.2.03, 10-19 October, 2002. + + + + + + Deep Space 1 + Mission + 1998-10-24 + 2001-12-18 + + The Deep Space 1 mission was a "new technology" mission that performed engineering + tests of various technologies, including io propulsion and autonomous navigation. + It also flew by asteroid (9660) Braille and Comet 19P/Borrelly. + + + diff --git a/data/pds4/context-pds4/investigation/mission.double_asteroid_redirection_test_2.0.xml b/data/pds4/context-pds4/investigation/mission.double_asteroid_redirection_test_2.0.xml new file mode 100644 index 00000000..79613415 --- /dev/null +++ b/data/pds4/context-pds4/investigation/mission.double_asteroid_redirection_test_2.0.xml @@ -0,0 +1,126 @@ + + + + + + urn:nasa:pds:context:investigation:mission.double_asteroid_redirection_test + 2.0 + Double Asteroid Redirection Test + 1.22.0.0 + Product_Context + + + DART + + + + + + 2024-08-03 + 2.0 + + Edited to comply with Editorial Working Group checklist. + + + + 2021-08-11 + 1.0 + + Created by A.C.Raugh based on descriptions from the DART Data Management and Archive Plan. + + + + + + + + urn:nasa:pds:context:agency:agency.nasa + context_to_associate + investigation_to_agency + + + + urn:nasa:pds:context:instrument_host:spacecraft.dart + investigation_to_instrument_host + + + urn:nasa:pds:context:instrument_host:spacecraft.liciacube + investigation_to_instrument_host + + + + urn:nasa:pds:context:investigation:mission.light_italian_cubesat_for_imaging_of_asteroids + context_to_associate + + The LICIACube mission by the Agenzia Spaziale Italiana (ASI) is running concurrently with the DART mission. + + + + + urn:nasa:pds:context:facility:observatory.lowell + investigation_to_facility + + + urn:nasa:pds:context:telescope:lowell.discovery_4m3 + investigation_to_telescope + + + + urn:nasa:pds:context:facility:observatory.las_campanas + investigation_to_facility + + + urn:nasa:pds:context:telescope:las_campanas.magellan_baade_6m5 + investigation_to_telescope + + + + urn:nasa:pds:context:facility:observatory.magdalena_ridge + investigation_to_facility + + + urn:nasa:pds:context:telescope:magdalena_ridge.mro2m4 + investigation_to_telescope + + + + urn:nasa:pds:context:facility:observatory.las_cumbres + investigation_to_facility + + + urn:nasa:pds:context:telescope:las_cumbres.2m0_telescopes + investigation_to_telescope + + + + urn:nasa:pds:context:target:asteroid.65803_didymos + investigation_to_target + Primary of the Didymos system + + + urn:nasa:pds:context:target:satellite.65803_didymos.dimorphos + investigation_to_target + + Secondary of the Didymos system, and the impact target for this spacecraft. + + + + + urn:nasa:pds:context_support:document:dart_description + investigation_to_document + + + + + Mission + 1000-01-01 + + + The DART mission was a planetary defense and technology demonstration mission that + impacted the moon (Dimorphos) of the Didymos asteroid system to measure the effect + on the moon's orbit. + + + diff --git a/data/pds4/context-pds4/investigation/mission.epoxi_2.0.xml b/data/pds4/context-pds4/investigation/mission.epoxi_2.0.xml new file mode 100644 index 00000000..f4c2e5b4 --- /dev/null +++ b/data/pds4/context-pds4/investigation/mission.epoxi_2.0.xml @@ -0,0 +1,169 @@ + + + + + + + urn:nasa:pds:context:investigation:mission.epoxi + 2.0 + EPOXI + 1.22.0.0 + Product_Context + + + Deep Impact Extended Investigation + + + DIXI + + + Extrasolar Planet Observation and Characterization + + + EPOCh + + + + + 2024-08-03 + 2.0 + + Edited to comply with Editorial Working Group checklist. + Updated deprecated target references with invalid LIDs + Removed inappropriate external references list. + + + + 2019-01-03 + 1.1 + + Per "Guide toPDS4 Context Products" v1.3, + - changed all lidvid_reference to lid_reference + - changed target LIDs to new formation rule + + + + 2016-10-01 + 1.0 + + extracted metadata from PDS3 catalog and + modified to comply with PDS4 Information Model + + + + + + + + urn:nasa:pds:context:agency:agency.nasa + context_to_associate + investigation_to_agency + + + urn:nasa:pds:context:instrument_host:spacecraft.dif + investigation_to_instrument_host + + + urn:nasa:pds:context_support:document:epoxi_description + investigation_to_document + + + urn:nasa:pds:context:target:calibrator.calibration + investigation_to_target + + + urn:nasa:pds:context:target:comet.103p_hartley_2 + instrument_host_to_target + + + urn:nasa:pds:context:target:comet.c2009_p1_garradd + investigation_to_target + + + urn:nasa:pds:context:target:comet.c2012_s1_ison + investigation_to_target + + + urn:nasa:pds:context:target:planet.earth + investigation_to_target + + + urn:nasa:pds:context:target:planet.mars + investigation_to_target + + + urn:nasa:pds:context:target:star.ross_905 + investigation_to_target + + + urn:nasa:pds:context:target:star.bd_36_2593 + investigation_to_target + + + urn:nasa:pds:context:target:star.bd_47_2846 + investigation_to_target + + + urn:nasa:pds:context:target:star.moa_2009-blg-266 + investigation_to_target + + + urn:nasa:pds:context:target:star.kepler-1 + investigation_to_target + + + urn:nasa:pds:context:target:star.1swasp_j175207.01_373246.3 + investigation_to_target + + + urn:nasa:pds:context:target:star.wasp-3 + investigation_to_target + + + urn:nasa:pds:context:target:star.xo-2 + investigation_to_target + + + urn:nasa:pds:context:target:star.xo-3 + investigation_to_target + + + + A'Hearn, M.F., EPOXI: Deep Impact Gets Glued to Extra-Solar Planets, 37th + COSPAR Scientific Assembly, Committee on Space Research, Montreal, Canada, 2008. + + + + + A'Hearn, M.F., J.M. Sunshine, L.A. McFadden, D.D. Wellnitz, D.D., L.M. Feaga, + T.L. Farnham, J.-Y. Li, M.J.S. Belton, P.C. Thomas, J. Veverka, and K.P. + Klaasen, EPOXI's Mission to Comet 103P/Hartley 2, 10th Asteroids, Comets, + Meteors Meeting, The Johns Hopkins University Applied Physics Laboratory, + Baltimore, Maryland, USA, 2008. + + + + 10.1109/AERO.2009.4839704 + + Rieber, R.R., and R.F. Sharrow, The Contingency of Success: Operations for Deep + Impact's Planet Hunt, Aerospace Conference, 2009 IEEE, pages 1-9, 7-14 March + 2009, doi:10.1109/AERO.2009.4839704. + + + + + + EPOXI + Mission + 2007-09-26 + 2013-09-20 + + + "EPOXI" was the monniker assigned to the two extended missions for the Deep + Impact Spacecraft: EPOCh, an exoplanet observation mission; and DIXI, the + extended mission to Comet 103P/Hartley 2. + + + diff --git a/data/pds4/context-pds4/investigation/mission.giotto_2.0.xml b/data/pds4/context-pds4/investigation/mission.giotto_2.0.xml new file mode 100644 index 00000000..5ce6c291 --- /dev/null +++ b/data/pds4/context-pds4/investigation/mission.giotto_2.0.xml @@ -0,0 +1,68 @@ + + + + + + + urn:esa:psa:context:investigation:mission.giotto + 2.0 + Giotto + 1.22.0.0 + Product_Context + + + 2024-08-03 + 2.0 + + Edited to comply with Editorial Working Group checklist. + + + + 2021-02-24 + 1.0 + + Changed LIDs from urn:nasa:pds: to urn:esa:psa: + + + + + + + + urn:nasa:pds:context:agency:agency.esa + context_to_associate + investigation_to_agency + + + urn:esa:psa:context:instrument_host:spacecraft.gio + investigation_to_instrument_host + + + urn:nasa:pds:context:target:comet.1p_halley + investigation_to_target + + + urn:nasa:pds:context_support:document:giotto_description + investigation_to_document + + + The Giotto Mission, R. Reinhard and B. Battrick, ESA SP-1077, ESA Pub Div, Noordwijk, Netherlands, 1986. + + + Reinhard, R., 'The Giotto Mission to Halley's Comet', in Exploration of Halley's Comet, edited by M. Grewing, F. Praderie, and R. Reinhard, Springer-Verlag, (Berlin), p950, 1988. + + + + + GIOTTO + Mission + 1985-07-02 + 1992-07-10 + + + The Giotto mission to comet 1P/Halley was the first mission to return close-up images + of a comet nucleas, and also the first deep-space mission flown by the European Space + Agency. + + + diff --git a/data/pds4/context-pds4/investigation/mission.hayabusa_3.0.xml b/data/pds4/context-pds4/investigation/mission.hayabusa_3.0.xml new file mode 100644 index 00000000..3af9c9c7 --- /dev/null +++ b/data/pds4/context-pds4/investigation/mission.hayabusa_3.0.xml @@ -0,0 +1,121 @@ + + + + + + urn:nasa:pds:context:investigation:mission.hayabusa + 3.0 + Hayabusa Mission + 1.22.0.0 + Product_Context + + + hay + hay + + + MUSES-C + + + Mu Space Engineering Spacecraft C + + + + + 2024-08-09 + 3.0 + + Edited to comply with Editorial Working Group checklist. + Updated alias list. + Found unlinked mission description, updated, but submitted to + context support collection to hold until it is determined if it + is feasible to update it in the mission bundle. + + + + 2016-10-01 + 1.0 + Extracted metadata from PDS3 catalog and modified to + comply with PDS4 Information Model. + + + 2019-01-03 + 1.1 + Per "Guide toPDS4 Context Products" v1.3, - changed all lidvid_reference to lid_reference - changed target LIDs to new formation rule + + + 2022-08-10 + 2.0 + Custom update by K. Lopez (SBN) to improve information and + metadata. + + + + + + urn:nasa:pds:context:agency:agency.jaxa + context_to_associate + investigation_to_agency + + + urn:nasa:pds:context_support:document:hayabusa_description + investigation_to_document + + + urn:nasa:pds:context:instrument_host:spacecraft.hay + instrument_to_instrument_host + + + urn:nasa:pds:context:instrument:amica.hay + instrument_host_to_instrument + + + urn:nasa:pds:context:instrument:lidar.hay + instrument_host_to_instrument + + + urn:nasa:pds:context:instrument:nirs.hay + instrument_host_to_instrument + + + urn:nasa:pds:context:target:asteroid.25143_itokawa + investigation_to_target + + + 10.1111/j.1945-5100.2001.tb01950.x + Binzel, R.P., A.S. Rivkin, S.J. Bus, J.M. Sunshine, T.H. Burbine, MUSES-C target asteroid (25143) 1998 SF36: A reddened + ordinary chondrite, Meteoritics and Planetary Science 36, 1167-1172, 2001. + + + 10.1126/science.1125841 + Fujiwara, A., J. Kawaguchi, D.K. Yeomans, M. Abe, T. Mukai, and 17 others, The rubble-pile asteroid Itokawa as observed + by Hayabusa, Science 312, 1330-1334, 2006. + + + 10.2322/tstj.7.Tb_1 + Kuninaka, Hitoshi, K. Nishiyama, Y. Shimizu, T. Yamada, and H. Koizumi, Re-ignition of Microwave Discharge Ion Engines + on Hayabusa for Homeward Journey, The 30th International Electric Propulsion Conference, Florence, Italy, Sept. 17-20, 2007. + + + 10.1126/science.1126164 + Yano, H., T. Kubota, M. Miyamoto, T. Okada, D. Scheeres, and 15 others, Touchdown of the Hayabusa spacecraft at the Muses + Sea on Hayabusa, Science 312, 1350-1353, 2006. + + + + Hayabusa Mission + Mission + 2003-05-09 + 2010-06-13 + + The Hayabusa (formerly MUSES-C) mission was a JAXA mission that + successfully returned samples from asteroid (25143) Itokawa to + Earth. The spacecraft itself burned up on reentry into Earth's + atmosphere, as planned. + + + diff --git a/data/pds4/context-pds4/investigation/mission.infrared_astronomical_satellite_3.0.xml b/data/pds4/context-pds4/investigation/mission.infrared_astronomical_satellite_3.0.xml new file mode 100644 index 00000000..30af67ff --- /dev/null +++ b/data/pds4/context-pds4/investigation/mission.infrared_astronomical_satellite_3.0.xml @@ -0,0 +1,82 @@ + + + + + + + urn:nasa:pds:context:investigation:mission.infrared_astronomical_satellite + 3.0 + Infrared Astronomical Satellite + 1.22.0.0 + Product_Context + + + IRAS + + + + + 2024-08-09 + 3.0 + + Edited to comply with Editorial Working Group checklist. + Added missing DOIs for references. + + + + 2016-10-01 + 1.0 + Extracted metadata from PDS3 catalog and modified to comply with PDS4 Information Model + + + 2022-08-28 + 2.0 + Custom update by K. Lopez (SBN) to improve information and + metadata. + + + + + + + urn:nasa:pds:context:agency:agency.nasa + context_to_associate + investigation_to_agency + + + urn:nasa:pds:context:instrument_host:spacecraft.iras::1.0 + investigation_to_instrument_host + + + urn:nasa:pds:context_support:iras_description + investigation_to_document + + + Beichman, C.A., G. Neugebauer, H.J. Habing, P.E. Clegg, and T.J. Chester, 1988, Infrared Astronomical Satellite Catalog and Atlases, Volume 1, Explanatory Supplement, NASA RP-1190. + + + 10.1086/184209 + Neugebauer, G., H.J. Habing, R. van Duinen, H.H. Aumann, B. Baud, C.A. Beichman, D.A. Beintema, N. Boggess, P.E. Clegg, T. de Jong, J.P. Emerson, T.N. Gautier, F.C. Gillett, S. Harris, M.G. Hauser, J.R. Houck, R.E. Jennings, F.J. Low, P.L. Marsden, G. Miley, F.M. Olnon, S.R. Pottasch, E. Raimond, M. Rowan-Robinson, B.T. Soifer, R.G. Walker, P.R. Wesselius, and E. Young, The Infrared Astronomical Satellite (IRAS) Mission, Astrophysica Journal 278, L1-L6, 1984. + + + 10.1086/184210 + Rowan-Robinson, M., P.E. Clegg, C.A. Beichman, G. Neugebauer, B.T. Soifer, H.H. Aumann, D.A. Beintema, N. Boggess, J.P. Emerson, T.N. Gautier, F.C. Gillett, M.G. Hauser, J.R. Houck, F.J. Low, and R.G. Walker, 1984, The IRAS minisurvey, AJ, 278, L7-L10. + + + + + Infrared Astronomical Satellite + Mission + 1983-01-26 + 1983-11-23 + + The IRAS mission was a joint program of the USA, the Netherlands, and the UK + to conduct a survey of the sky in four IR wavelengths. It also made pointed + observatons of selected astronomical and solar system objects. + + + diff --git a/data/pds4/context-pds4/investigation/mission.international_cometary_explorer_2.0.xml b/data/pds4/context-pds4/investigation/mission.international_cometary_explorer_2.0.xml new file mode 100644 index 00000000..3d107bf1 --- /dev/null +++ b/data/pds4/context-pds4/investigation/mission.international_cometary_explorer_2.0.xml @@ -0,0 +1,88 @@ + + + + + + + urn:nasa:pds:context:investigation:mission.international_cometary_explorer + 2.0 + International Sun-Earth Explorer-3/International Cometary Explorer + 1.22.0.0 + Product_Context + + + ISEE-3/ICE + + + ICE + + + + + 2024-08-09 + 2.0 + + Edited to comply with Editorial Working Group checklist. + Corrected minor typo in reference. + + + + 2019-01-03 + 1.1 + + Per "Guide toPDS4 Context Products" v1.3, + - changed all lidvid_reference to lid_reference + - changed target LIDs to new formation rule + + + + 2016-10-01 + 1.0 + + extracted metadata from PDS3 catalog and + modified to comply with PDS4 Information Model + + + + + + + + urn:nasa:pds:context:agency:agency.nasa + context_to_associate + investigation_to_agency + + + urn:nasa:pds:context_support:document:ice_description + investigation_to_document + + + urn:nasa:pds:context:instrument_host:spacecraft.ice + investigation_to_instrument_host + + + urn:nasa:pds:context:target:comet.21p_giacobini-zinner + investigation_to_target + + + + Reinhard, R and B. Battrick (eds), 'Space Missions to Halley's Comet', European + Space Agency ESA SP-1066, ESA Pub Div, Noordwijk, Netherlands, 1986. + + + + + + International Sun-Earth Explorer-3/International Cometary Explorer + Mission + 1983-12-22 + 1997-05-05 + + + The ICE mission renamed and redirected the ISEE-3 spacecraft to fly by + Comet 21P/Giacobini-Zinner. It was the first spacecraft to fly by a comet. + + + diff --git a/data/pds4/context-pds4/investigation/mission.iue_2.0.xml b/data/pds4/context-pds4/investigation/mission.iue_2.0.xml new file mode 100644 index 00000000..166ae519 --- /dev/null +++ b/data/pds4/context-pds4/investigation/mission.iue_2.0.xml @@ -0,0 +1,94 @@ + + + + + + urn:esa:psa:context:investigation:mission.iue + 2.0 + International Ultraviolet Explorer + 1.22.0.0 + Product_Context + + + IUE + + + + + 2024-08-19 + 1.0 + + Creation + + + + 2021-02-25 + 1.0 + + Changed LIDs from urn:nasa:pds: to urn:esa:psa: + And per "Guide toPDS4 Context Products" v1.7, + changed all lidvid_reference to lid_reference + + + + + + + + urn:nasa:pds:context:agency:agency.nasa + context_to_associate + investigation_to_agency + + + urn:nasa:pds:context:agency:agency.esa + context_to_associate + investigation_to_agency + + + urn:esa:psa:context:instrument_host:spacecraft.iue + investigation_to_instrument_host + + + urn:nasa:pds:context_support:document:iue_description + investigation_to_document + + + + The Science and Engineering Research Council of the United Kingdom + + + This agency was the third collaborator, with NASA and ESA, in the + developement and operation of the IUE spacecraft and mission. + + + + 10.1038/275377a0 + + Boggess, A., Bohlin, R.C., Evans, D.C., Freeman, H.R., Gull, T.R., Heap, + S.R., Klinglesmith, D.A., Longanecker, G.R., Sparks, W., West, D.K., Holm, + A.V., Perry, P.M., Schiffer III, F.H., Turnrose, B.E., Wu, C.C., Lane, + A.L., Linsky, J.L., Savage, B.D., Benvenuti, P., Cassatella, A.,Clavel, + J., Heck, A., Macchetto,F., Penston, M.V., Selvelli, C.I., Dunford, E., + Gondhaleker, P., Oliver, M.B., Sandford, M.C.W., Stickland, D., + Boksenberg, A., Coleman, C.I., Snijders, M.A.J., Wilson, R., In-Flight + Performance of the IUE, Nature, 275, 377, 1978. + + + + + + International Ultraviolet Explorer + Mission + 1978-01-26 + 1996-09-30 + + + The IUE mission observed all types of astronomical objects, + from comets to quasars, in UV wavelengths (1200-3350 Andstromgs). + It operated continuously in a geosynchronous orbit over the + period January 1978 to September 1996. + + + diff --git a/data/pds4/context-pds4/investigation/mission.mariner71_2.0.xml b/data/pds4/context-pds4/investigation/mission.mariner71_2.0.xml new file mode 100644 index 00000000..8d2330e0 --- /dev/null +++ b/data/pds4/context-pds4/investigation/mission.mariner71_2.0.xml @@ -0,0 +1,241 @@ + + + + + + urn:nasa:pds:context:investigation:mission.mariner71 + 2.0 + Mariner Mars '71 + 1.22.0.0 + Product_Context + + + MM '71 + + + MARINER71 + + This identification appears to be unique to PDS. + + + + + + 2024-08-19 + 1.0 + + Edited to comply with Editorial Working Group checklist. + + + + 2016-10-01 + 1.0 + + extracted metadata from PDS3 catalog and + modified to comply with PDS4 Information Model + + + + + + + + urn:nasa:pds:context:agency:agency.nasa + context_to_associate + investigation_to_agency + + + urn:nasa:pds:context:instrument_host:spacecraft.mr9::1.0 + investigation_to_instrument_host + + + urn:nasa:pds:context:target:planet.mars::1.0 + investigation_to_target + + + urn:nasa:pds:context_support:document:mm71_description + investigation_to_document + + + + Mariner Mars 1971 Project Final Report, Science Experiment Reports, JPL + Technical Report 32-1550, Vol. V, Aug. 20, 1973. + + Also available as: + Mariner Mars 1971 project. Volume 5: Science experiment reports, NASA + Technical Reports Server (NTRS), Document ID 19730025101, Accession + Number 73N33834. + + + + + + Mariner Mars '71 + Mission + 1971-05-08 + 1972-10-27 + + + The Mariner Mars '71 project launched two spacecraft, Mariners + 8 and 9, to orbit Mars. Mariner 8 was lost at launch. Mariner + 9, launched 30 May 1971, succeeded in reaching and orbiting Mars. + + + Mission Overview + ================ + On November 14, 1971, Mariner 9 became the first spacecraft to + orbit another planet. Six experiments were carried as part of + the science payload: television, ultraviolet spectrometer, + infrared spectroscopy, infrared radiometry, S-band occultation + and celestial mechanics. Two experiments (S-band occultation + and celestial mechanics) utilized the radio telemetry subsystem + to derive data; the other required specially developed + instruments, mounted, and boresighted to each other, on the + spacecraft's scan platform. Pre-launch mission planning + encompassed two separate, but complementary, missions. The + orbit of each spacecraft was optimized to match the + corresponding objective. The mapping mission was designed with + an Earth-synchronous orbit (about a 12-hr periods) to maximize + antenna utilization, or communications efficiency. For maximum + surveillance of an area, it was designed with a steep + inclination (80 degrees) to the equatorial plane of Mars. The + dynamic objective dictated a Mars-synchronous (or + sub-synchronous) orbit and a lower (50 degree) inclination for + closer observations of specific areas. The plans for the two + missions were in detailed stages of development on May 9, 1971 + when Mariner 8 was lost because of guidance difficulties in the + second stage of the launch vehicle. It was determined that an + orbit for a single-spacecraft mission could be developed to meet + all basic mission and specific science objectives. A + single-spacecraft plan, involving an inclination of 65 degrees, + a period of about 12 hours, a periapsis altitude of 1350 Km, and + an arrival date of November 14, 1971, was evaluated and + formalized in 2 weeks. + + + Mariner 9 Statistics + -------------------- + + Total mission 516 days + Required minimum useful orbital lifetime - 90 days + Actual useful orbital lifetime - 349 days + Distance from Earth to Mars on 10/27/72 - 383,675,000Km + Commands received by Mariner 9 - 45,960 + TV pictures received of Mars and its satellites - 7329 + TV shutter actuations - 14,004 + Required minimum mapping coverage - 70% of planet + Actual mapping coverage obtained - 100% of planet + Science data received from Mariner 9 - 54 billion bits + + + Mariner 9 'firsts' + ------------------ + + 1. Orbit another planet, + 2. Detail observation of Martian Atmospheric Changes, + 3. Complete mapping of another planet, + 4. Detail observations of satellites of another planet, + 5. Observation by spacecraft of receding polar cap. + + + Mariner 9 'Discoveries' + ----------------------- + + 1. Tectonic action on Mars (Crust movement), + 2. Existence of volcanoes and lava flows, + 3. Evidence of past fluid flow, + 4. Eolian activity (wind erosion and deposition), + 5. Rough gravity field, + 6. Triaxiality of Mars, + 7. Evidence of process of differentiation of Mars similar to + that of Earth, + 8. Permanent residual polar cap. + + On October 28, 1972, Mariner 9 ran out of attitude control gas + and was commanded to be silent for the final time. It is + estimated that Mariner 9 will remain in Mars orbit for more + than 50 years. + + + Mission Phases + ============== + + CRUISE + ------ + On June 5th, a planned trajectory correction was made. + Martian ephemeris data and spacecraft tracking calculations + were determined with such accuracy that no other midcourse + corrections were necessary during the 167 day flight to Mars. + Other events during cruise were scan calibration no. 1 on + October 1, scan calibration no. 2 on October 8, Mars TV + calibration on November 8 and November 9. + + Spacecraft Id : MR9 + Target Name : MARS + Mission Phase Start Time : 1971-05-30 + Mission Phase Stop Time : 1971-11-14 + Spacecraft Operations Type : ORBITER + + + LAUNCH + ------ + Mariner 9 was successfully launched from Cape Kennedy, Florida + at 6:23 PM EDT. The Centaur-Mariner 9 separation occurred at + 6:36 PM EDT. + + Spacecraft Id : MR9 + Target Name : MARS + Mission Phase Start Time : 1971-05-30 + Mission Phase Stop Time : 1971-05-30 + Spacecraft Operations Type : ORBITER + + + ORBITAL + ------- + The 1398 Km periapsis altitude of the insertion orbit was + accurate to with 50 Km from the aiming point, and the initial + period of 12 hr and 34 min was within seconds of the time + desired for the insertion orbit. The non-synchronization with + Earth provided the timing slip until coincidence of the + Goldstone 64-m antenna zenith position and orbit periapsis was + obtained and a trim maneuver 'locked' the two into + synchronization. On November 16, the spacecrafts' orbital + period was changed by more than 30 min by a 6-sec firing of + the rocket engines. However, because of the previously + unknown gravity-field variation of the planet the average + orbital period was found to be slightly shorter that the + 11:58:52 planned, gradually changing the time relationship of + periapsis to the view period of the 64-m antenna at Goldstone, + California, which would eventually affect data playbacks. On + December 30 (revolution 94), a second trim maneuver adjusted + the orbital period, correcting periapsis-passage timing with + the view period of the 64-m antenna. This new orbit + established a higher periapsis altitude, which provided a + broader area coverage for each television picture, thus + requiring fewer picture to complete the desired mapping of 70% + of the surface during the standard 90 day mission. The + broader area coverage for each pictured resulted in a + corresponding loss of surface resolution. About 122 days + after orbit insertion, the pointing direction of the + spacecraft's high-gain antenna drifted off of Earth, and + communications became more difficult. A high-gain antenna + maneuver (HGAM) of the spacecraft became necessary to point + the antenna to Earth. On October 27, 1972, telemetry data + indicated that the spacecraft was no longer capable of holding + the fixed attitude and, as the last battery power was being + used, a final command was sent to stop transmitting. The + slowly tumbling Mariner 9 will remain in orbit for a minimum + of 50 years before it enters the atmosphere of Mars, + disintegrates, and falls to the surface. + + Spacecraft Id : MR9 + Target Name : MARS + Mission Phase Start Time : 1971-11-14 + Mission Phase Stop Time : 1979-10-27 + Spacecraft Operations Type : ORBITER + + + + diff --git a/data/pds4/context_support/bundle.xml b/data/pds4/context_support/bundle.xml new file mode 100644 index 00000000..0d985202 --- /dev/null +++ b/data/pds4/context_support/bundle.xml @@ -0,0 +1,44 @@ + + + + + + urn:nasa:pds:context_support + 1.0 + Context Product Support Bundle + 1.22.0.0 + Product_Bundle + + 2024 + + The collections in the bundle provide supporting documents, images, + graphics, and similar information to support browsing for and + displaying information about archival data. + + + + + 2024-08-01 + 1.0 + + Creation + + + + + + Supplemental + + + urn:nasa:pds:context_support:document::1.0 + Primary + bundle_has_document_collection + + + urn:nasa:pds:context_support:image::1.0 + Primary + bundle_has_document_collection + + \ No newline at end of file diff --git a/data/pds4/context_support/document/RosettaMissionCatalog.txt b/data/pds4/context_support/document/RosettaMissionCatalog.txt new file mode 100644 index 00000000..6a090d96 --- /dev/null +++ b/data/pds4/context_support/document/RosettaMissionCatalog.txt @@ -0,0 +1,2690 @@ +PDS_VERSION_ID = PDS3 +LABEL_REVISION_NOTE = " + 2002-10-21 JV: INITIAL DRAFT + 2002-10-22 JJZ: MISSION_PHASE_INFORMATION OBJECT ADDED + 2004-09-23 KW: Partly updated. MISSION_PHASE_INFORMATION + removed. + 2005-09-19 KW: Added INSTRUMENT_HOST_ID RL. + 2005-12-09 AC: two MISSION_HOST, one for each inst_host + updated MISSION_DESC, + added MISSION_TARGET objects, + changed MISSION_STOP_DATE to NULL + added References + 2006-01-12 AC: removed special characters + 2006-01-23 AC: removed double quotes within description + 2007-01-26 MB: update to 70 char line length + 2008-02-05 MB: TBD updates + 2008-05-27 MB: TBD updates + 2009-11-24 MB: REF (GLASSMEIER), STEINS + 2010-01-18 MB: Non ascii characters + 2010-01-20 MB: GULKIS ref + 2010-02-10 IR: GLASSMEIER REF 2007B + added + 2010-02-24 MB: EAR3 updated + 2010-03-25 MB: PC12 addition + 2010-08-25 MB: REF updates. + 2011-02-18 MB: REF updates (KISSSEL) + 2011-03-31 MB: REF RO-EST-RP-3226 removed + 2011-06-06 MB: editorial after RPC MIP delta review + 2012-01-30 MB: AST2 and RVM1 description + 2012-03-12 MB: typo line 2081 + 2012-06-05 Maud Barthelemy after AST2 review + 2015-01-30 Maud Barthelemy after Wake up and Landing + 2015-02-27 Maud Barthelemy slight updates + 2015-03-02 Maud Barthelemy Ref updates + 2015-08-18 Maud Barthelemy updates for new Lander Acronyms + 2017-09-18 Maud Barthelemy updates on mission dates + 2017-11-17 Maud Barthelemy typo corrections + 2018-02-27 Maud Barthelemy RPC MIP description + 2018-02-27 Maud Barthelemy typo corrections + " + +RECORD_TYPE = STREAM + +OBJECT = MISSION + MISSION_NAME = "INTERNATIONAL ROSETTA MISSION" + + OBJECT = MISSION_INFORMATION + MISSION_ALIAS_NAME = ROSETTA + MISSION_START_DATE = 1995-03-01 + /* THIS IS THE ANNOUNCEMENT OF OPPORTUNITY DATE [RO-EST-AO-0001] */ + MISSION_STOP_DATE = "NULL" + + MISSION_OBJECTIVES_SUMMARY = " + The prime scientific objective of the Rosetta mission + is to study the origin of comets, the relationship + between cometary and interstellar material and its + implications with regard to the origin of the Solar + System. " + + MISSION_DESC = " + + +TABLE OF CONTENTS +---------------------------------- += ROSETTA Mission Overview += ROSETTA Mission Objectives + - Science Objectives += Mission Profile += Mission Phases Overview + - Mission Phase Schedule + - Solar Conjunctions/Oppositions + - Payload Checkouts += Mission Phases Description + - Launch phase (LEOP) + - Commissioning phase + - Cruise phase 1 + - Earth swing-by 1 + - Cruise phase 2 (and Deep Impact) + - Mars swing-by + - Cruise phase 3 + - Earth swing-by 2 + - Cruise phase 4 (splitted in 4-1 and 4-2) + - Steins flyby + - Earth swing-by 3 + - Cruise phase 5 + - Lutetia flyby + - Rendez-Vous Manoeuver 1 + - Cruise phase 6 + - Rendez-Vous Manoeuver 2 + - Near comet drift (NCD) phase + - Approach phase + - Lander delivery and relay phase + - Escort phase + - Near perihelion phase + - Extended mission += Orbiter Experiments + - ALICE + - CONSERT + - COSIMA + - GIADA + - MIDAS + - MIRO + - OSIRIS + - ROSINA + - RPC + - RSI + - VIRTIS + - SREM += LANDER (PHILAE) + - Science Objectives + - Lander Experiments += Ground Segment + - Rosetta Ground Segment + - Rosetta Science Operations Center + - Rosetta Mission Operations Center + - Rosetta Lander Ground Segment + - Lander Control Center + - Science Operations and Navigation Center + - Rosetta Scientific Data Archive + += Acronyms + + +ROSETTA Mission Overview +===================================================================== + +The ROSETTA mission is an interplanetary mission whose main +objectives are the rendezvous and in-situ measurements of the comet +67P/Churyumov-Gerasimenko, scheduled for 2014/2015. The spacecraft +carries a Rosetta Lander, named Philae, to the nucleus and deploys it +onto its surface. + +A brief description of the mission and its objectives can be found in +[GLASSMEIERETAL2007A]. A detailed description of the mission analysis +can be found in the ROSETTA User Manual [RO-DSS-MA-1001], and the +flight Operations Plan [RO-ESC-PL-5000]. + +On its long way to the comet nucleus after a Launch by Ariane 5 P1+ +in March 2004, the ROSETTA spacecraft orbited the Sun for one year +until it returned to Earth for the first swing-by. The planet Mars was +reached in February 2007, about 3 years after launch. In November +2007 a second Earth swing-by took place and a third one in November +2009. Two asteroid flybys (2867 Steins and 21 Lutetia) were performed +on the way to the comet. These two asteroids had been selected at the +Science Working Team meeting on 11th March 2004 among all the +available candidate asteroids, depending on the scientific interest +and the propellant required for the correction manoeuvre. Around the +aphelion of its orbit, which is 5.3 AU from the Sun, the spacecraft +has been in a spinning hibernation mode for about 2.5 years. + +Rosetta rendezvoused with comet 67P/Churyumov-Gerasimenko in August +2014. The Philae lander was deployed to the surface of the comet on 12 +November 2014. +The end of the nominal mission is planned in December 2015. +The mission has been extended to 30th September 2016. + +The Mission Phase Schedule can be found below based on the official +mission calendar. For archive purpose, we used a slightly updated +calendar splitting the escort and extension phases. +Below we summarise the phases used by the team for archive purpose: + +MISSION_PHASE_NAME | Abbn | Start date | End date | +-------------------------------------------------------------- +'GROUND' | GRND | *** | 2019-09-30 | +'LAUNCH' | LEOP | 2004-03-03 | 2004-03-04 | +'COMMISSIONING 1' | CVP1 | 2004-03-05 | 2004-06-06 | +'CRUISE 1' | CR1 | 2004-06-07 | 2004-09-05 | +'COMMISSIONING 2' | CVP2 | 2004-09-06 | 2004-10-16 | +'EARTH SWING-BY 1' | EAR1 | 2004-10-17 | 2005-04-04 | +'CRUISE 2' | CR2 | 2005-04-05 | 2006-07-28 | +'MARS SWING-BY ' | MARS | 2006-07-29 | 2007-05-28 | +'CRUISE 3' | CR3 | 2007-05-29 | 2007-09-12 | +'EARTH SWING-BY 2' | EAR2 | 2007-09-13 | 2008-01-27 | +'CRUISE 4-1' | CR4A | 2008-01-28 | 2008-08-03 | +'STEINS FLY-BY' | AST1 | 2008-08-04 | 2008-10-05 | +'CRUISE 4-2' | CR4B | 2008-10-06 | 2009-09-13 | +'EARTH SWING-BY 3' | EAR3 | 2009-09-14 | 2009-12-13 | +'CRUISE 5' | CR5 | 2009-12-14 | 2010-05-16 | +'LUTETIA FLY-BY' | AST2 | 2010-05-17 | 2010-09-03 | +'RENDEZVOUS MANOEUVRE 1' | RVM1 | 2010-09-04 | 2011-06-07 | +'CRUISE 6' | CR6 | 2011-06-08 | 2014-01-20 | +'PRELANDING' | PRL | 2014-01-21 | 2014-11-19 | +'COMET ESCORT 1' | ESC1 | 2014-11-20 | 2015-03-10 | +'COMET ESCORT 2' | ESC2 | 2015-03-11 | 2015-06-30 | +'COMET ESCORT 3' | ESC3 | 2015-07-01 | 2015-10-21 | +'COMET ESCORT 4' | ESC4 | 2015-10-22 | 2015-12-31 | +ROSETTA EXTENSION 1 | EXT1 | 2016-01-01 | 2016-04-05 | +ROSETTA EXTENSION 2 | EXT2 | 2016-04-06 | 2016-06-30 | +ROSETTA EXTENSION 3 | EXT3 | 2016-07-01 | 2016-09-30 | +-------------------------------------------------------------- + +For the Lander, the Cruise Phase data sets followed the same +filenaming but the Comet phase has been split differently: + +MISSION_PHASE_NAME | Abbn| Start date | End date | +---------------------------------------------------------------------- +'POST HIBERNATION | PHC | 2014-04-09T08:15:25 | 2014-04-23T15:45:13 | + COMMISSIONING' | | | | +---------------------------------------------------------------------- +'PRE DELIVERY | PDCS| 2014-07-13T14:42:56 | 2014-10-17T20:31:20 | + CALIB SCIENCE' | | | | +---------------------------------------------------------------------- +'SEPARATION DESCENT| SDL | 2014-11-12T08:35:02 | 2014-11-12T15:34:04 | + LANDING' | | | | +---------------------------------------------------------------------- + 'REBOUNDS' | RBD | 2014-11-12T15:34:05 | 2014-11-12T17:30:20 | +---------------------------------------------------------------------- +'FIRST SCIENCE | FSS | 2014-11-12T17:30:21 | 2014-11-15T01:00:00 | + SEQUENCE' | | | | +---------------------------------------------------------------------- + +Please note: +------------ +The ROSETTA spacecraft was originally designed for a mission to the +comet 46 P/Wirtanen to be launched in January 2003. Due to a delay of +the launch a new comet (67P/Churyumov-Gerasimenko) had been selected +by the Science Working Team on 3rd-4th April 2003. +The compliance of the design was checked and where necessary adapted +for this new mission. Therefore in the following all the details and +characteristics for this new mission are used. + + +ROSETTA Mission Objectives +===================================================================== + +The scientific objectives of the ROSETTA mission can be considered +from three main viewpoints: + +First of all, comets and asteroids are fully-fledged members of our +solar system, which means, that they are objects of intrinsic +interest to planetary scientists. The level of investigations +conducted on these bodies is therefore far below that achieved for +the other objects of the solar system. +The study of the small solar-system bodies arguably represents the +last major gap in the tremendous worldwide effort that has been made +to reveal our planetary neighbours to us. + +The most important scientific rationale for studying small solar- +system bodies is the key role-play in helping us to understand the +formation of the solar system. Comets and asteroids have a close +genetic relationship with the planetesimals, which formed from the +solar nebula 4.57 billion years ago. Most of our present +understanding of these processes has been obtained by studying +meteorites, which constitute a biased sample of asteroidal material, +and micrometeoroids, which may represent cometary grains processed by +solar radiation and atmospheric entry. There is therefore a strong +scientific case of studying cometary material in situ, as it is +surely more primitive than extraterrestrial samples. + +A third scientific aspect is the study of the physio-chemical +processes, which are specific to comets and asteroids. In this +respect, asteroids can provide information on impact phenomena, +particularly on very large scale. However, the increase in cometary +activity as these bodies approach the Sun undoubtedly represents one +of the most complex and fascinating processes to be observed in the +solar system. + +Science Objectives +--------------------- +The prime scientific objectives as defined in the Announcement of +Opportunity [RO-EST-AO-0001] by the Rosetta Science Team can be +summarized as: + +- Global characterisation of the nucleus, determination of dynamic +properties, surface morphology and composition + +- Chemical, mineralogical and isotropic compositions of volatiles and +refractories in a cometary nucleus + +- Physical properties and interrelation of volatiles and refractories +in a cometary nucleus + +- Study of the development of cometary activity and the processes in +the surface layer of the nucleus and in the inner coma (dust-gas +interaction) + +- Origin of comets, relationship between cometary and interstellar +material. + +- Implications for the origin of the solar system + +- Global characterisation of the asteroid, determination of dynamic +properties, surface morphology and composition. + + +Mission Profile +===================================================================== + +The ROSETTA mission profile results from the orbit of the target +comet 67P/Churyumov-Gerasimenko, which has a perihelion close to 1.2 +AU and an aphelion of about 5.7 AU, resulting in a period of about +6.5 years. A detailed description of the Mission Profile can be found +in the Rosetta Mission Calendar [RO-ESC-PL-5026] and in the RSOC +Design Specification [RO-EST-PL-2010]. + +The injection of the spacecraft by a single Ariane 5 Launch with the +so-called 'delayed ignition' of the upper stage, was not directly into +the trajectory to the comet, because of the high spacecraft wet mass. +Therefore the spacecraft had to be accelerated by a sequence of +gravity assist manoeuvres at Mars and the Earth, in order to catch up +with the comet's velocity at perihelion. + +The initially large distance to the comet at the perihelion of its +trajectory has been slowly decreasing after the third Earth swing-by. +At the intersection of both orbits, the difference in orbit +inclination and the residual relative velocity were diminished by the +comet orbit matching manoeuvre at around 4.0 AU Sun distance. The +range of the spacecraft-to-Sun distance was between 0.88 and 5.33 AU, +defined by the minimum Sun distance during the first five years of the +mission with the swing-bys at Earth, and the maximum Sun distance +close to the aphelion of the comet's orbit. The evolution of the +spacecraft distance to Earth over the mission time followed the +profile of the Sun distance superimposed by an oscillation with an +amplitude of 2 AU (+1,-1) and a period of about one year due to the +Earth's motion around the Sun. This resulted in a range from 0 AU +(Earth Departure and Swing-by) to 6.3 AU during the superior solar +conjunction close to the spacecraft's aphelion (see Solar Conjunctions +section below). + +After the second and third Earth swing-by ROSETTA crossed the +asteroid main belt, which gave the opportunity of two asteroid flybys. +The asteroids 2867 Steins and 21 Lutetia, were encountered on +5 September 2008 and 10 July 2010 respectively. These two asteroids +had been selected at the Science Working Team meeting on 11th March +2004 among all the available candidate asteroids, depending on the +scientific interests and the propellant required for the correction +manoeuvre. +Between the major mission events, up to the comet rendezvous +manoeuvre, the spacecraft performed long interplanetary cruise phases +(up to 2.5 years) with several solar conjunctions (see Solar +Conjunctions section below) and the power critical aphelion passage +(last cruise phase). In order to reduce the ground segment costs and +the wear and tear of spacecraft equipment during these phases, the +spacecraft was put in 'Hibernation Mode'. + +Two types of hibernation modes were planned to be used: + +* 'Deep Space Hibernation Mode' above 4.5 AU: Inertial spin mode with +a spin rate of 4 deg/sec. The spacecraft was almost entirely passive, +except of receivers/ decoders, power supply, heaters and two +Processor Modules with one RTU. + +* 'Near Sun Hibernation Mode' below 4.5 AU: 3-axes stabilised mode +with the solar arrays Sun-pointing and the +X-axis Earth-pointing. +Attitude control was performed with thrusters and star trackers, based +on ephemerides; occasional solar array adjustments and ground +contacts via the medium gain antenna (MGA). + +The final approach to the comet into its sphere of influence was +prepared by the rendezvous manoeuvre (RVM-2), that matched the +spacecraft orbit with the comet orbit. + +A subsequent sequence of approach manoeuvres, supported by optical +navigation, took the spacecraft closer and closer to the comet. +After determination of the physical model of the comet by Doppler and +optical measurements, the spacecraft was inserted into a global +mapping orbit around the comet. + +The 'Duck-shape' of the comet was a surprised and a challenge for the +Flight Dynamics team. Three activity cases had been planned to orbit +the comet, respectively at 30, 20 or 10km. Finally, it has been chosen +to go to 10km. +Meanwhile, a board was selecting 5 and then 2 landing sites. The +chosen landing site were located on the 'head' of the Duck Shape +comet. +The delivery of the Lander or Surface Science Package (SSP) was +achieved from an eccentric orbit, which took the spacecraft to a low +altitude above the selected landing site. The Lander release was fully +automatic according to a predefined schedule, and led to a first touch +down with minimum vertical and horizontal velocities relative to the +local rotating surface. +The first touch down reached the foreseen landing site within 50m +accuracy. However, the Lander did not succeed in harpooning and +bounced twice. It was stopped by cliff walls, which unluckily hid the +Lander from the Sun. +The Lander, Philae, had the time to operate all instruments on board, +during a phase named the FSS, First Science Sequence, before going to +sleep on November, 15th at 00:36 UTC. Upon the landing of the Lander, +the spacecraft provided uplink and downlink data relay between the +Lander and the Earth. + +After the Lander delivery the ROSETTA spacecraft escorted the comet +until the perihelion passage (13th August 2015) and outwards again, +until a Sun distance of 2 AU was reached at end of the year 2015. +The main scientific objective during this phase was the monitoring of +the features of the active comet. +The mission was extended from 1st January 2016 to 30th September 2016. +Rosetta ended its journey on September 30th by a controlled impact +onto the comet from a altitude of about 19km. + +Mission Phases Overview +====================================================================== + +This section gives an overview of the major mission phases and main +events in scheduled tables. A description of the individual phases is +given in the following section. More detailed information can be +found in the Rosetta Mission Calendar [RO-ESC-PL-5026] and the RSOC +Design Specification [RO-EST-PL-2010] + +Mission Phase Schedule +----------------------- +The following table shows a schedule of the mission phases, with +start-end times (dd/mm/yyyy), duration (days) and distance to the sun +(Astronomical Units). Some of the most important events within the +mission phases are marked with an arrow (->). Further description of +each mission phase is given below. + +.==================================================================== +| Phase |Start Date|Main Event| End Date |Dur |SunDist(AU)| +|=================|==========|==========|==========|====|===========| +|LEOP |02/03/2004| |04/03/2004| 3 | | +|-----------------|----------|----------|----------|----|-----------| +|Commissioning1 |05/03/2004| |06/06/2004| 94 | 0.89-0.99 | +| ->DSM1 | |11/05/2004| | | | +| ->DSM1 Touch-up| |16/05/2004| | | | +|-----------------|----------|----------|----------|----|-----------| +|Cruise 1 |07/06/2004| |05/09/2004| 91 | 0.89-1.04 | +|-----------------|----------|----------|----------|----|-----------| +|Commissioning2 |06/09/2004| |16/10/2004| 41 | 1.04-1.09 | +|-----------------|----------|----------|----------|----|-----------| +|Earth Swing-by1 |17/10/2004| |04/04/2005| 170| 0.99-1.11 | +| ->Earth | |04/03/2005| | | | +|-----------------|----------|----------|----------|----|-----------| +|Cruise 2 |05/04/2005| |28/07/2006| 480| 1.04-1.76 | +| ->Deep Impact | |04/07/2005| | | | +|-----------------|----------|----------|----------|----|-----------| +|Mars Swing-by |29/07/2006| |28/05/2007| 304| 0.99-1.59 | +| ->DSM2 | |29/09/2006| | | | +| ->Mars | |25/02/2007| | | | +| ->DSM3 | |29/04/2007| | | | +|-----------------|----------|----------|----------|----|-----------| +|Cruise 3 |29/05/2007| |12/09/2007| 107| 1.32-1.58 | +|-----------------|----------|----------|----------|----|-----------| +|Earth Swing-by2 |13/09/2007| |27/01/2008| 137| 0.91-1.32 | +| ->Earth | |13/11/2007| | | | +|-----------------|----------|----------|----------|----|-----------| +|Cruise 4-1 |28/01/2008| |03/08/2008| 189| 1.02-2.03 | +|-----------------|----------|----------|----------|----|-----------| +|Steins Flyby |04/08/2008| |05/10/2008| 63 | 2.03-2.19 | +| ->Steins | |05/09/2008| | | | +|-----------------|----------|----------|----------|----|-----------| +|Cruise 4-2 |06/10/2008| |13/09/2009| 343| 1.35-2.26 | +| ->DSM4 | |19/03/2009| | | | +|-----------------|----------|----------|----------|----|-----------| +|Earth Swing-by3 |14/09/2009| |13/12/2009| 92 | 0.98-1.35 | +| ->Earth | |13/11/2009| | | | +|-----------------|----------|----------|----------|----|-----------| +|Cruise 5 |14/12/2009| |16/05/2010| 154| 1.03-2.45 | +|-----------------|----------|----------|----------|----|-----------| +|Lutetia Flyby |17/05/2010| |03/09/2010| 111| 2.45-3.14 | +| ->Lutetia | |10/07/2010| | | | +|-----------------|----------|----------|----------|----|-----------| +|Rendez-vousMan1 |04/09/2010| |13/07/2011| 313| 3.15-4.58 | +| ->RVM1 | |23/01/2011| | | | +|-----------------|----------|----------|----------|----|-----------| +|Cruise 6 (DSHM) |14/07/2011| |20/01/2014| 917| 4.46-5.29 | +|-----------------|----------|----------|----------|----|-----------| +|Rendez-vousMan2 |21/01/2014| |17/08/2014| 206| 3.40-4.49 | +| ->RVM2 1st burn | |21/05/2014| | | | +|-----------------|----------|----------|----------|----|-----------| +|Global Mapping |18/08/2014| |19/10/2014| 63 | 3.15-3.53 | +|and Close | | | | | | +|Observation | | | | | | +|-----------------|----------|----------|----------|----|-----------| +|Lander Delivery |20/10/2014| |16/11/2014| 28 | 2.97-3.15 | +|->Lander Delivery| |12/11/2014| | | | +|-----------------|----------|----------|----------|----|-----------| +|Comet Escort |17/11/2014| |31/12/2015| 410| 1.24-2.96 | +'-------------------------------------------------------------------' +| Extension |31/12/2015| |30/09/2016| 274| 2.01-3.83 | +'-------------------------------------------------------------------' + +Payload Checkouts +----------------- +Payload checkouts were scenarios designed to allow Rosetta payload to +make regular health checks, to activate mechanisms and to monitor +trends through calibration tests. They were allocated in the mission +calendar at regular 6-month periods during the first 10 years of the +mission cruise phase. They were split into passive and active payload +checkouts. Passive payload checkouts were entirely non-interactive. +Conditions for the passive checkout were that it would: +a) not require any real time monitoring, b) run entirely off of MTL, +c) not require s/c specific pointing other than to maintain listed +constraints, d) produce minimal science data. Active payload checkout +operations were executed both interactively and non-interactively . +Conditions for the active checkout were that it would: a) limit the +requirement for real time monitoring, b) run mostly from MTL, c) limit +the requirement for s/c specific pointing beyond maintaining listed +constraints, d) produce minimal science data. There was more +flexibility during active checkouts and in addition payloads used +interactive passes to make any necessary memory patches and tests. + +.-------------------------------------------------------------------. +| Name | Type | Begin | End | Mission Phase | +|-----------------|--------|----------|-----------|-----------------| +| P/L Checkout 0 |Passive |27/03/2005| 31/03/2005| Earth Swing-by 1| +| P/L Checkout 1 |Passive |30/09/2005| 05/10/2005| Cruise 2 | +| P/L Checkout 2 |Passive |03/03/2006| 08/03/2006| Cruise 2 | +| P/L Checkout 3 |Passive |25/08/2006| 30/08/2006| Mars Swing-by | +| P/L Checkout 4 | Active |23/11/2006| 22/12/2006| Mars Swing-by | +| P/L Checkout 5 |Passive |18/05/2007| 23/05/2007| Mars Swing-by | +| P/L Checkout 6 | Active |13/09/2007| 29/09/2007| Earth Swing-by 2| +| P/L Checkout 7 |Passive |04/01/2008| 09/01/2008| Earth Swing-by 2| +| P/L Checkout 8 | Active |19/07/2008| 24/07/2008| Cruise 4-1 | +| P/L Checkout 9 |Passive |28/01/2009| 02/02/2009| Cruise 4-2 | +| P/L Checkout 10 | Active |18/09/2009| 08/10/2009| Earth Swing-by 3| +| P/L Checkout 12 |Passive |22/04/2010| 15/05/2010| Cruise 5 | +| P/L Checkout 13 |Passive |01/12/2010| 15/12/2010| RVM1 | +'-------------------------------------------------------------------' + +Solar Conjunctions/Oppositions +------------------------------- +Other mission phases, which resulted from the orbit geometry and +interfered with the above operational phases, were the solar +conjunctions. +Two types of conjunctions occurred throughout the mission: + +* Solar Oppositions: The Earth was between spacecraft and Sun, +resulting in a degradation of the command link to the spacecraft. + +* Superior Solar Conjunctions: Sun was between spacecraft and Earth, +resulting in a degradation of the command and telemetry link to/from +the spacecraft. + +Table below shows the solar conjunction phases throughout the mission +with type, begin and duration of the conjunction and corresponding +mission phase. The phases are defined as the periods, during which +the Sun-SpaceCraft-Earth (SSCE) angle is below 5 degrees. + +.-------------------------------------------------------------------. +| Type |Duration| Begin | End | Mission Phase | +|---------------|--------|------------|------------|----------------| +| Conjunction 1 | 48d | 21/03/2006 | 07/05/2006 | Cruise 2 | +| Conjunction 2 | 39d | 08/12/2008 | 15/01/2009 | Cruise 4-2 | +| Conjunction 3 | 50d | 22/09/2010 | 10/11/2010 | RV Manoeuver 1 | +| Opposition 1 | 37d | 13/04/2011 | 19/05/2011 | RV Manoeuver 1 | +| Conjunction 4 | 64d | 15/10/2011 | 17/12/2011 | Cruise 6 | +| Opposition 2 | 47d | 30/04/2012 | 15/06/2012 | Cruise 6 | +| Conjunction 5 | 67d | 31/10/2012 | 05/01/2013 | Cruise 6 | +| Opposition 3 | 46d | 20/05/2013 | 04/07/2013 | Cruise 6 | +| Conjunction 6 | 60d | 24/11/2013 | 22/01/2014 | Cruise 6 | +| Opposition 4 | 28d | 25/06/2014 | 22/07/2014 | RV Manoeuver 2 | +| Conjunction 7 | 41d | 21/01/2015 | 02/03/2015 | Comet Escort | +'-------------------------------------------------------------------- + +It can be noted that for archive purpose and because of the non +expected landing, which included rebounds, the Lander team provided +the data sets from wake up up to the First Science Sequence (FSS) in 5 +data sets with sub mission phases that differ from the official ones. +The table below lists these sub phases: + +---------------------------------------------------------------------- +| PHC | Post Hibernation | 2014-04-09T08:15:25 | 2014-04-23T15:45:13| +| | Commissioning | | | +|------|------------------|---------------------|--------------------| +| PDCS | Pre Delivery | 2014-07-13T14:42:56 | 2014-10-17T20:31:20| +| | Calib Science | | | +|------|------------------|---------------------|--------------------| +| SDL | Separation | 2014-11-12T08:35:02 | 2014-11-12T15:34:04| +| | Descent Landing | | | +|------|------------------|---------------------|--------------------| +| RBD | Rebounds | 2014-11-12T15:34:05 | 2014-11-12T17:30:20| +|------|------------------|---------------------|--------------------| +| FSS | First Science | 2014-11-12T17:30:21 | 2014-11-15T01:00:00| +| | Sequence | | | +---------------------------------------------------------------------- + +The Orbiter instruments use the phase Prelanding (PRL) to deliver the +data from wake-up to FSS. + +Mission Phases Description +===================================================================== + +Launch and Early Orbit Phase (LEOP) +----------------------------- +Rosetta was launched by an Ariane 5/G+ in a dedicated flight (single +launch configuration) from Kourou at 07:17:51 UTC 2 March 2004. After +burnout of the lower composite, the upper stage together with the +spacecraft remained in an eccentric coast arc for nearly 2 hours. +Then the upper stage performed delayed ignition and injected the +Rosetta spacecraft into the required escape hyperbola. + +After spacecraft separation from the upper stage, Rosetta acquired +its three axes stabilised Sun pointing attitude and deployed the solar +arrays autonomously. Ground operations acquired the down-link in +S-band using the ESA network and controlled the spacecraft to a fine- +pointing attitude with the HGA pointing towards Earth using X-band +telemetry. Tracking and orbit determination were performed, the +departure trajectory was verified and corrected by the on-board +propulsion system of the spacecraft. + +The launch locks of the Lander Philae were released at the end of the +first ground station pass. Philae remained firmly attached to the +spacecraft by the cruise latches until its release at the comet. + +Commissioning phase (1 and 2) +------------------- +Commissioning started three days after launch following the first +trajectory correction manoeuvre. A Deep Space Manoeuver (DSM1) of 173 +m/s was executed at perihelion. All spacecraft functions needed during +the cruise to the comet, in particular for hibernation, were checked +and the scientific payload was commissioned. + +Commissioning was done in two parts, as the New Norcia ground station +must have been shared with Mars Express and could not be used +by Rosetta from June to mid-September 2004. + +For more information refer to the following reports: +[RO-EST-RP-3293] Consolidated Rosetta Payload Report of the Mission +Commissioning Results Review +[RO-EST-RP-3307] RSOC_Commissioning_Results_Report_2005Dec19.pdf +[RO-EST-RP-3343] Interference Scenario Report + +Cruise phase 1 +-------------- +Almost all the scientific instruments, except ALICE were switched off +while ground contact was practically not available. No payload +operations were done during this phase. + +Earth swing-by 1 +---------------- +The actual Earth swing-by took place on 4-Mar-05. The phase ended one +month after the swing-by and the spacecraft was prepared for the next +cruise phase to Mars. +One passive Payload Checkout was scheduled end of March 2005. +Immediately after this flyby an Asteroid Flyby Mode Simulation was +performed using the Moon as a target. Some limited payload operations +were permitted shortly before during and shortly after this Earth +Flyby. Rosetta payload teams were given the opportunity to conduct +scientific investigation that included close approach of both the +Earth and the Moon and the AFM simulation. Any activities that did not +require the Earth-Moon system i.e. continued instrument commissioning, +were considered for later in the Mission, such as during the next +active checkout. + +The instrument objectives are listed below. + +ORBITER + + ALICE + - Flat field calibration + - Extended object scattered light calibration (Moon as the target) + - Absolute solar calibration + - Absolute flux and wavelength calibration (wide part of the slit + to take in the Moon) + - Door performance test due to anomalies raised during + commissioning + + MIRO + - Asteroid Flyby Simulation test + - H2O lines in Earth (high quality data obtained but analysis not + complete) + - Radiometric calibration of the Moon + + RPC + - Sensor calibration + - Magnetospheric physics + - Verification of the science operations modes for the Mars flyby + + RSI + - HGA to Earth around closest approach to Moon + + OSIRIS + - Because of technical issues OSIRIS was not operated during the + Earth Swing-By itself. + + + VIRTIS + - Co-alignment M/H + - Aldebaran target in IR (failed, boresight did not detect the + target) + - Absolute calibration using the Moon + - Full disc Earth imaging including exosphere over one rotation + +LANDER + + CIVA + - Earth Picture with Camera #2 or 4 + + ROMAP with RPC MAG + - magnetic axes alignment of sensors with Earth magnetic field + - Checking of scaled values with known Earth values + - Solar wind values comparison with other s/c + + +Problems: + + RPC + - Loss of LAP science data for 41.5 hours (2005-03-01 19:00 -- + 2005-04-03 12:30). +For more information refer to the following reports: +[RO-EST-RP-3318] Payload Passive Checkout 0 Report +[RO-EST-RP-3321] Rosetta Earth-Swingby #1 Payload Operations Report + +Cruise phase 2 (and Deep Impact) +-------------------------------- +After leaving the Earth, the spacecraft made one revolution around the +Sun, and in the second arc from perihelion to aphelion made a swing-by +of Mars. + +There was a solar conjunction for more than one month in April 2006 +(see Solar Conjunctions section above). Two passive check-outs with +non-interactive instrument operations for about 5 days were scheduled +during the cruise to Mars. PC1 occurred from 5/09/2005 to 5/10/2005. +PC2 took place from 3/03/2006 to 8/03/2006. + +The NASA Deep Impact mission encountered comet 9P/Tempel 1 on 4 July +2005, which fell into the Cruise 2 mission phase. At around 06:00 +UTC, the mother probe sent a 362 kg impactor into the nucleus with a +relative speed of 10.2 km/s. Rosetta was in a privileged position for +its remote sensing instruments to observe the event (80 million km +distance, 90 degrees angle respect to the sun). Rosetta monitored +Tempel 1 continuously (i.e. 24 hrs per day) over an extended period +from 7 days before the deep impact to 11 days afterwards (27Jun-15Jul +2005). The first 2 days ALICE observed the stars for calibration. From +the 28th June to the 15th July, OSIRIS, ALICE, and MIRO operated +observing comet 9P/Tempel 1 continuously. VIRTIS was on only several +hours around the impact. Maintenance activities were carried out for +COSIMA, ROSINA, ALICE. + +During the Deep Impact subphase, the instruments had the following +objectives: + +ORBITER + + ALICE + - Baseline pre-impact spectrum. Comparison with near and long + term post impact spectra. The comet was detected in all spectra. + - Strong atomic lines of neutral H and O were detected throughout + the observation period. + - Two weak lines of neutral C detected on some dates. No change + detected by ALICE in comet's UV spectrum as a result of impact + - except for possible enhancement in C emission. + - No evidence of Ar, S, N, CO. + - Water production rates. Results TBC. + - Dark histograms. + - Calibration star before the encounter. Spectra of calibration + star was used for calibration of the Deep Impact spectra and + instrument sensitivity. The data was also used to look for any + flux variations due to pointing/jitter (initial results did not + show any evidence of significant fluctuations in the stellar + count rate). + - Memory patch (time synchronisation issue). + + MIRO + - Changes in the coma composition induced by the impact. + - Upper limit on the water production rate in the pre-impact + phase of the experiment. Water production rate and albeit + with low signal-to-noise measured in the post impact phase. The + water production rate was less than had been anticipated based + on models. + - Detection of carbon monoxide: the analysis was not complete but + so far no CO was detected. + - Estimate of Doppler velocity. + + OSIRIS + - Accurate photometry of the unresolved nucleus (no atmosphere in + between) with complete time coverage. The time resolution was + better than a minute around the impact and could draw conclusion + about the evolution of the impact cloud during the first hour. + The long term monitoring allowed determination of the composition + and evolution of the impact cloud (water production and dust/ice + ratio) + - UV coverage that allowed imaging of the OH emission at 308nm + (estimate of the water production by the impact) + - Imaging of the coma out to at least 150000km from the nucleus. + The effect of the impact could be seen in the images for + approximately a week (stereo reconstruction of coma, + impact cloud). + + VIRTIS + - Coma and ejecta composition and temporal evolution. But the + outburst due to the impact was not energetic enough to reach the + minimum sensitivity required. + +Conclusions of the Deep Impact Observations: + +The science objectives of the Deep Impact Observations scenario were +met. The brightness increase of Tempel 1 produced by the impact was +lower than we had hoped for, and as a result the comet was too weak to +be detected by VIRTIS. For ALICE and MIRO the signal was just above +the sensitivity limit, but nevertheless important measurements could +be achieved. The results of OSIRIS even exceeded the expectations, and +the first scientific publications were widely cited. The data +collected by the experiments on board Rosetta are unique because +Tempel 1 was monitored continuously over an extended period of time +(no day-and-night cycle in contrast to ground-based telescopes) and in +the absence of an absorbing atmosphere. + +The following operations was done during the Passive checkout 1: + +ORBITER + + ALICE + - Electronic and software + - Test pattern and stim test + - Memory check + - dark exposures + There was no instrument anomalies. The door performance test + showed nominal behavior. + + CONSERT + - Consert Orbiter verification + - Consert Lander verification + - Consert Orbiter/Lander time synchronisation + + COSIMA + - Self check + - Target manipulator unit maintenance + - Ion emitter maintenance + + GIADA + - Run mechanisms - cover operations + - Health check (all subsystems, electronics, noise and + contamination monitoring, performances estimation) + + MIDAS + - Exercising of all mechanisms (shutter, approach mechanism, + linear stage, wheel, scanner) + The test was successful and MIDAS is fully operable. + + MIRO + - Regular exercise and health check of all commands in all modes + - Regular dump of EEPROM memory to check for radiation damage. + All objectives were met. There was no radiation damage of the + EEPROM. + + RPC + - MAG: instrument calibration. Undisturbed solar wind was measured + to calibrate the offsets of the MAG instrument in quiet conditions + (Hedgecock method). + - LAP: instrument calibration. + - MIP: Instrument checkout + - IES: measurement in the undisturbed solar wind for calibration + of its sensors and cross calibration with LAP. + The PC operations were completed successfully with no change in + instrument performance for MAG and IES. + + RSI + Two frequency downlink driven by the USO and a ground station + that could receive the X and S band signals. + - Investigate the stability of the USO + - Verify interaction with the ground + Investigations of the USO data from PC#0 revealed that the + behaviour of the USO was obviously not as good as it had been + during the last USO test in October. + + OSIRIS + - Exercise the instrument mechanisms + - Verify the sanity of the CCD + - Verify the focus + No anomaly occurred. + + +LANDER + Test of the Lander Platform overall performance + Secondary battery monitoring + Lander extended AFT + CDMS EEPROM dump + functional test for + PTOLEMY + CONSERT + +The following operations have been done during the Passive checkout 2: + +ORBITER + + ALICE + - same health tests as PC1. Tests successful. + + CONSERT + - same as PC1. Tests generally successful (see report) + + COSIMA + - self check of all hardware sub-systems on operational voltage + levels + - target manipulator unit checkout + - maintenance COSISCOPE checkout + - emitter maintenance + Tests generally successful. + + GIADA + - Same as PC1 plus monitoring of MBS coating evolution. + The cover operations went fine. There was no further contamination + of the microbalances. GDS is not fully tested for light + conditions. IS seems nominal. All HK values were as expected. + + MIDAS + - same as PC1. Tests were successful. + + MIRO + - Same as PC1. Overall success. + + RPC + - Same as PC1. All performances checked were nominal. + + RSI + - Same as PC1. The USO behaved very good, USO drift satisfactory. + + OSIRIS + - Same as PC1. Generally successful. For solar elongation + angles < 90 degrees OSIRIS got substantial scattered light + through the nominally closed doors. The scattered light observed + during PC2 was unfortunately enough that parts of the CCD surface + was saturated. This happened in spite of the large exposure time + reduction that was made after PC1. + + VIRTIS + - The check done were performed properly. + +LANDER + Same as PC1 plus functional tests for + MUPUS + CONSERT + +For more information refer to the following reports: +[RO-EST-RP-3341] Deep Impact Observations, Payload Operations Report +[RO-EST-RP-3342] Passive Payload Checkout 1 Report +[RO-EST-RP-3418] Passive Payload Checkout 2 Report + +Mars swing-by +------------- +The mission phase began two months before DSM2 of 65 m/s, which was +performed near perihelion. The actual Mars swing-by took place on +25-Feb-07. The minimum altitude with respect to the Martian surface +was 200 km. The relative approach and departure velocity was 8.8 km/s. +During the swing-by a communications black-out of approximately 14 +min was expected due to occultation of the spacecraft by Mars. +Furthermore the spacecraft was expected to be in eclipse for about 24 +min. The phase ended one month after DSM3. DSM3 of 129 m/s was +scheduled near the aphelion of this arc in order to obtain the proper +arrival conditions at the Earth. Two passive payload check-outs of +about 5 days and an active longer one of 25 days were scheduled during +the phase (PC3, PC4, PC5). + +PC3 started on 25th August 2006 and ended 30th August 2006. +The following operations were planed during PC3. GIADA and ROSINA did +not take part in this PC. + +ORBITER + ALICE + - Electronics & software verification, test pattern and stim test, + Memory Check, Aperture Door, Performance Test. + All operations are executed as expected. + + CONSERT + - Consert Orbiter verification, Consert Lander verification, + Consert Orbiter/Lander time Synchronisation. + + COSIMA + - self check of all hardware sub-systems on operational voltage + levels, target manipulator unit checkout and maintenance emitter + maintenance + + MIDAS + - Regular health check and exercising of all mechanisms (shutter, + approach mechanism, linear stage, wheel, scanner) + + MIRO + - Regular exercise and health check of all commands in all modes. + Regular dump of EEPROM memory to check for radiation damage. + All operations are successful. + + RPC + - MAG: Instrument calibration. Undisturbed solar wind measurement. + Such data will be used to calibrate the offsets of the MAG + instrument in quiet conditions (Hedgecock method). + - LAP: Instrument calibration. + - MIP: Instrument checkout. + - IES: measurements in the undisturbed solar wind for calibration + of its sensors and crosscalibration with LAP. + + RSI + - Investigate the stability of the USO and verify interaction + with the ground. + The PC3 results were very promising and the behavior of the USO + is as good as expected. The stability of the USO was still one + order of magnitude better than anticipated before launch. + + OSIRIS + - Instrument mechanisms, verify the sanity of the CCD, verify the + focus of the instrument. + + VIRTIS + - Both VIRTIS M and H were working as expected. + - PC3 was used to verify the upload of a new pixel map for + VIRTIS-H to be used during the forthcoming PC4 (pixel map allowed + to drastically reduce the data volume). + +LANDER + - Test of the Lander platform to check the overall performance and + Secondary Battery Status + - Lander Extended AFT with short function + - tests of some units and + EEPROM + - checks for all ComDPU units + - Secondary Battery Monitoring + - CDMS EEPROM dump + - Separate short functional tests for MUPUS and CONSERT + +PC4 was an active checkout. It started on Nov., 23rd and ended on +Dec., 22nd 2006. All Rosetta payload instruments took part in this +scenario. + +ALICE + - Passive Check out + - Optics Decontamination + - HV and detector tests + - Calibrations, performance + - Stare observations of Saturn and Vega + +CONSERT + - Passive 6 months Status Check + +NAVCAM + - Calibration + +COSIMA + - Maintenance Procedure + - Cosiscope operation + +GIADA + - Passive 6 months status check + - Settings test + +LANDER + - Lander interactive and non interactive operations + +MIDAS + - Check out and mechanism activation + - s/w upload and functional check out + - Calibration + - High resolution image of a dust collector facet + +MIRO + - Passive Status Check + +ROSINA + - DPU s/w Patch + - COPS microtips + - DFMS cover and modes + - RTOF delta commissioning + +RPC + - Passive Check out and calibrations + - IES noisy channels test, upload patches and tables + - LDL failure investigation + - Upload new LAP macros + - MIP new seq test + - Mars Swing By rehearsal + - ROMAP/RPC co operation + - MAG continuous operation + - Upload temporary patch for directional resolution improvement + +RSI + - Passive two frequency downlink + +SREM + - Continuous operation + +OSIRIS + - Passive 6 months Check + - Bias, darks, charge transfer efficiency with doors closed + - Patch s/w + - Staring observations + - Calibration and Mars Fly By preparation + +VIRTIS + - H and M calibrations + +Although several open issues were resolved in this checkout, several +issues remain open and new anomaly report were generated. +75% of the planned operations were successful. The 25% loss was mainly +due to OSIRIS that lost the majority of its operations. + +PC5 is a Passive Check Out that started on May, 18th and ended on May, +23rd 2007. The instruments that took part in this PC are listed below: +ALICE, CONSERT, COSIMA, GIADA, LANDER, MIDAS, MIRO, RPC, RSI, OSIRIS. +VIRTIS was NOGO and did not operate. +Main objectives of the scenario have been met with no issues. + +Payload checkout reports: +[RO-SGS-RP-0001] +_Rosetta_Passive_Payload_Checkout_3_Report_2007Jun27.pdf +[RO-EST-RP-3464] +_Rosetta_Report_Active_Payload_Checkout_4_2006Apr13.pdf +[RO-SGS-RP-0002] +_Rosetta_Passive_Payload_Checkout_5_Report_2007June27.pdf + +Cruise phase 3 +-------------- +No check-outs were scheduled during the short cruise to Earth. + +Earth swing-by 2 +---------------- +Daily operations started again around two months before Rosetta +reached Earth with tracking and navigation manoeuvres. The actual +Earth swing-by took place on 13-Nov-07. The perigee altitude was +13890 km. The relative approach and departure velocity was 9.3 km/s. +The phase ended one month after the LGA strobing phase. In this phase +the spacecraft got very close to the sun (min distance 0.91AU). One 15 +day payload checkout and one 5 day payload checkout were also +scheduled in this phase (PC6 and PC7). + +Payload Checkout 6 (PC6) was an active checkout where a target +independent opportunity to perform interactive operations and to +request spacecraft pointing was given to all Rosetta payload teams. +The active payload checkout 6 ran for 15 consecutive days starting on +the 13th September 2007 until the 29th September 2006. +All Rosetta payload took part in this scenario. Operations ranged from +a repeat of established passive checkout operations to extensive +software patching and calibration campaigns. Four instruments required +active spacecraft pointing during the scenario with nine different +targets observed. Pointing types were 7 stares, 2 slew scans, 2 raster +scans giving a total of around 176 hours of dedicated spacecraft +pointing. These were mostly for calibration purposes. +Overall operations went smoothly. Although several open issues were +resolved in this checkout several issues remained open and new ones +have been generated. + +Payload Checkout 7 (PC7) was a passive checkout run form 4th January +2008 to 9th January 2008. Main objectives have been met with no issue +apart from GD. This issue was due to higher operating temperatures +resulting from the short Sun-Spacecraft distance. + +The Payload checkout reports are: +[RO-SGS-RP-0004] +_Rosetta_Report_Active_Payload_Checkout_6_2007Oct30.doc +[RO-SGS-RP-0005] +_Rosetta_Passive_Payload_Checkout_7_Report_2008Jun24.pdf. + +Cruise phase 4 (split into 4-1 and 4-2) +-------------- +In this phase the spacecraft made one revolution around the Sun. +A solar conjunction took place in January 2009 (see Solar Conjunctions +section above), together with another two conjunctions of the Earth- +spacecraft- Sun angle (Sun-Earth conjunction as seen from the +spacecraft). In this phase the spacecraft got very close to the sun +(min distance 0.91AU). This Cruise phase has been splitted in two +parts after the selection of the first Asteroid flyby which fell +in the middle of this phase. Cruise 4-1 was before the flyby phase, +and 4-2 was right after. Two passive check-outs were scheduled, one +during Cruise 4-1 and the second one during Cruise 4-2. + +During CR4, Passive Checkout 9 and Active Checkout 8 were planned. + +Payload Checkout 8 (PC8) was an active checkout where a target +independent opportunity to perform interactive operations and to +request spacecraft pointing was given to all Rosetta payload teams. +All Rosetta payload took part in this scenario. +The Active Payload Checkout 8 ran for 2 days (05-06 July 2008) plus 26 +consecutive days starting on the 9th July 2008 until the 1st August +2008. +Three instruments required active spacecraft pointing during the +scenario with 9 different targets observed. Pointing types were 14 +stares and 3 raster scans. These were mostly for calibration purposes. + +Payload Checkout 9(PC9) was a passive checkout executed between 28th +January and 2nd February 2009. An RSI passive checkout was also +completed on 09th February. All but 2 of the Rosetta payload +instruments participated in the scenario, the exceptions being Rosina +and Virtis. Operations were limited to instrument health checks and +passive checkouts, as is the case for nominal Passive Checkout +scenarios. All of the operations planned and executed in the PC09 +scenario were successful (as detailed in Section 3). Minor issues were +observed by 2 instruments (CN and RS) but none of these prevented the +successful completion of the corresponding operations. + +The Payload checkout reports are: +[RO-SGS-RP-0019] +_Rosetta_Report_Active_Payload_Checkout_8_2011Jul25.pdf +[RO-SGS-RP-0030] +_Rosetta_Report_Passive_Payload_Checkout_9_2011Jul20.pdf + + +Steins flyby +------------- +Asteroid Steins was the first dedicated scientific target of the +Rosetta mission. Closest approach was on 5 September 2008 at 18:38:22 +UTC. Rosetta flew at 800 km from asteroid Steins. For the first time a +European spacecraft flew next to an asteroid, performed an optical +navigation campaign, and autonomously tracked the asteroid by means of +its on board camera. + +The 2867 Steins E-type asteroid had been discovered on 4 November 1969 +by N. Chernykh. Its dimensions have been estimated by [KELLERETAL2010] +to 6.67 x 5.81 x 4.47 km3, corresponding to a spherical equivalent +radius of 2.65 km. Its sidereal rotation period has been estimated to +6.04681 +/- 0.00002h, its pole direction in ecliptic coordinates to +approximately Lambda = 250 deg and Beta = -89 deg with an error of +about 5 degrees [LAMYETAL2008]. Its albedo has been estimated to 0.3 +in the visible and 0.4 in the infrared, both by [KELLERETAL2010] and +[LAMYETAL2008]. + +The two asteroids Rosetta flew by are secondary science targets of the +Rosetta mission, with comet 67P/Churyumov-Gerasimenko being the +primary science target. Therefore, scientific measurements of Asteroid +(2867) Steins had highest priority. Some calibrations were also +performed during the flyby phase. + +The flyby geometry necessitated a flip in the spacecraft attitude +before closest approach. As a compromise between the incompatible +requirements to minimize the illumination of the -X and +-Y panels of +the spacecraft (flip as late as possible) and to minimize the impact +on the science observations (flip as early as possible), the +spacecraft flip was performed between 40 and 20 minutes before closest +approach. Rosetta's relative speed with respect to Steins was 8.6km/s. + +The heliocentric and geocentric distances of Rosetta during the Steins +flyby were 2.14 AU and 2.41 AU, respectively. The one way light travel +time was 20 minutes. + +The estimated accuracy of the determination of the position of Steins +in the plane perpendicular to the flight direction during the naviga- +-tion campaign was +/-2 kms for navigation with OSIRIS and +/-16 kms +for navigation with the NAVCAMs (from navigation slot on Sept. 4). For +the targeted passage through phase angle 0 at a distance of 1280 kms +from Steins, a positional offset of 2 kms would correspond to a +minimum phase angle of 0.1 degree. + +The following table shows an overview of the Steins Flyby scenario: + +------------------------------------------------------------------ +| Start Date | End Date | Operation | +------------------------------------------------------------------ +| 04/08/2008 | 04/09/2008 | Navigation campaign (astrometry) using| +| | | NAVCAM and OSIRIS NAC | +------------------------------------------------------------------ +| 01/09/2008 | 10/09/2008 | Scientific operations targeting the | +| | | asteroid | +------------------------------------------------------------------ +| 07/09/2008 | 04/10/2008 | Observation of gravitational | +| | | microlensing events in the galactic | +| | | bulge by OSIRIS | +------------------------------------------------------------------- + +The following table shows the observation results per instrument: +---------------------------------------------------------------------- +| Instrument| Title |Success| Comments | +---------------------------------------------------------------------- +| ALICE 01 | Alice optics | Yes | at the beginning and | +| | decontamination | | end of all scenarios | +|--------------------------------------------------------------------| +| ALICE 02 | Standard stellar flux | Yes | During major | +| | calibration using the AL| | scenarios | +| | narrow center boresight | | | +|--------------------------------------------------------------------| +| ALICE 03 | Standard stellar flux | Yes | During major | +| | calibration using the AL| | scenarios | +| | +X wide bottom boresight| | | +|--------------------------------------------------------------------| +| ALICE 04 | Dark exposures | Yes | Regular calibration | +|--------------------------------------------------------------------| +| ALICE 05 | Search for evidence of | Yes | No exosphere or coma | +| | exosphere/coma around | | found | +| | Steins | | | +|--------------------------------------------------------------------| +| ALICE 06 | Point at Steins to | Yes | First Spectrum of an | +| | obtain an FUV spectrum | | asteroid below 200nm | +|--------------------------------------------------------------------| +| ALICE 07 | Point to the Steins RA | Yes | | +| | and Dec at the mid point| | | +| | of AL 06 observation | | | +|--------------------------------------------------------------------| +| ALICE 08 | Point to the Steins RA | Yes | | +| | and Dec at the mid point| | | +| | of AL 05 observation | | | +|--------------------------------------------------------------------| +| ALICE 09 | Standard stellar flux | Yes | During major | +| | calibration using the AL| | scenarios | +| | -X wide top boresight | | | +|--------------------------------------------------------------------| +| COSIMA 01 | Image and expose D8 | No | TMU error | +| | substrate | | | +|--------------------------------------------------------------------| +| COSIMA 02 | Image all D8 substrates | No | Cancelled after | +| | and store it | | failure of CS 01 | +|--------------------------------------------------------------------| +| GIADA 01 | non nominal operational | Yes | | +| | configuration, i.e. only| | | +| | impact sensor on and | | | +| | cover closed | | | +|--------------------------------------------------------------------| +| LANDER 01 | Run MUPUS TEM mode | Yes | | +| | during periods with | | | +| | pronounced temperature | | | +| | changes | | | +|--------------------------------------------------------------------| +| LANDER 02 | Operate ROMAP in slow | Yes | Interference from | +| | mode and fast mode | | MUPUS detected | +| | during CA +/-30min | | | +|--------------------------------------------------------------------| +| LANDER 03 | CASSE measurements | Yes | | +| | during WOL with SW FM-2 | | | +|--------------------------------------------------------------------| +| LANDER 04 | Thermal test of SESAME | Yes | | +| | soles | | | +|--------------------------------------------------------------------| +| LANDER 05 | Operation of CASSE and | Yes | | +| | DIM in a dusty environ-| | | +| | -ment | | | +|--------------------------------------------------------------------| +| MIRO 01 | Observation of Steins | Yes | | +| | during approach | | | +|--------------------------------------------------------------------| +| MIRO 02 | Run Asteroid Mode | Yes | Pointing inaccuracy | +| | sequence at closest | | during Asteroid Flyby| +| | approach to Steins | | mode affects scienti-| +| | | | -fic output | +|--------------------------------------------------------------------| +| MIRO 03 | Observation of Steins | Yes | | +| | during Recession | | | +|--------------------------------------------------------------------| +| ROSINA 01 | Outgassing | Yes | | +|--------------------------------------------------------------------| +| ROSINA 02 | Single mass measurement | Yes | Contamination issue | +| | sequence | | due to s/c flip. | +| | | | Sw instability caused| +| | | | temporary switch-off | +| | | | of detector | +|--------------------------------------------------------------------| +| ROSINA 03 | Pressure monitoring | Yes | Contamination issue | +| | | | due to s/c flip | +|--------------------------------------------------------------------| +| RPC 01 | Steins Fly by | Mostly| ICA did not produce | +| | | | scientifically useful| +| | | | data due to a comman-| +| | | | -ding error. | +| | | | Interference from | +| | | | MUPUS detected | +|--------------------------------------------------------------------| +| RSI 01 | Coherent measurement | TBD | TBD | +| | with Xup/Xdown or Xup/ | | | +| | Sdown received by a | | | +| | groundstation capable of| | | +| | receiving X- and S- band| | | +| | Doppler and Ranging | | | +| | Signals | | | +|--------------------------------------------------------------------| +| SREM 01 | SREM standard | YES | No Steins specific | +| | accumulation | | operations, general | +| | | | particle flux | +| | | | monitoring | +|--------------------------------------------------------------------| +| OSIRIS 01 | Vega Stare | Yes | Stellar calibrations | +| | | | repeated during major| +| | | | scenarios | +|--------------------------------------------------------------------| +| OSIRIS 02 | 16 Cyg Stare | Yes | Stellar calibrations | +| | | | repeated during major| +| | | | scenarios | +|--------------------------------------------------------------------| +| OSIRIS 03 | Steins Lightcurve at | Yes | TBD | +| | CA-2 weeks | | | +|--------------------------------------------------------------------| +| OSIRIS 04 | Steins Lightcurve at | Mostly| WAC data compromised | +| | CA-24 hours | | by overexposure | +|--------------------------------------------------------------------| +| OSIRIS 05 | Steins observation at CA| Mostly| NAC went into Safe | +| | | | mode due to shutter | +| | | | issues about 10 min | +| | | | before CA | +|--------------------------------------------------------------------| +| OSIRIS 06 | Fast imaging sequence | Yes | observation merged | +| | around the time of phase| | with OSIRIS 05 | +| | angle 0 | | | +|--------------------------------------------------------------------| +| OSIRIS 07 | Characterization of | Yes | TBD | +| | solar straylight for | | | +| | same orientation as the | | | +| | one the s/c had when | | | +| | the OSIRIS hill sphere | | | +| | dust search was | | | +| | performed | | | +|--------------------------------------------------------------------| +| VIRTIS 01 | VIRTIS-M lightcurve of | Yes | TBD | +| | Steins | | | +|--------------------------------------------------------------------| +| VIRTIS 02 | V-M and V-H operating; | Yes | Operations were | +| |s/c stare at target Nadir| |affected by inaccuracy| +| | looking; continuous | | of s/c pointing | +| | acquisition in pushbroom| | | +| | mode | | | +|--------------------------------------------------------------------| +| VIRTIS 03 | V-M and V-H continuous | Yes | TBD | +| |observation of Steins for| | | +| | 1 hour after VR02; V-M | | | +| | in image mode (10 lines | | | +| | scan) | | | +|--------------------------------------------------------------------| + + +The Rosetta first asteroid flyby was a success. The navigation +campaign produced highly accurate predictions of the Steins position, +and during the flyby most instruments worked without serious problems. +Asteroid flyby mode worked well, although with somewhat lower tracking +accuracy than expected. + +Summary results per instrument during closest approach can be found in +the operation report: +[RO-SGS-RP-0020] Science Operations Report for the Steins FlyBy + +Earth swing-by 3 +---------------- +Operations were essentially the same as for the Earth swing-by 2. The +actual Earth swing-by took place in Nov-09. The perigee altitude was +300 km. The relative approach and departure velocity was 9.9 km/s. +Phase started 3 months before the swing-by and ends 1 month later. Two +short payload checkouts of about 5 days each were scheduled during +this phase. + +The phase contained the Active Payload Checkout 10 (PC10). The section +first describes PC 10 and then the Earth Flyby. + + PC10 + ---- + The Active PC10 ran for 18 consecutive days from 18th September 2009 + to 4th October 2009. It represented a target independent opportunity + to perform interactive operations and to request spacecraft + pointing. All payloads took part in this scenario, as interactive + or non-interactive operations. There were approximately 425 hours of + non-interactive and 68 hours of interactive operations. Four + instruments required active s/c pointing with 15 targets observed + (111 hours of dedicated s/c pointing). These were mostly for + calibration purposes. + + More details on the results can be found in the report: +[RO-SGS-RP-0022] Payload Report Active PC10 + + Earth flyby 3 (EAR3) + -------------- + This was the last of the three gravity assists from the Earth, after + which Rosetta increased its orbital energy, enough to allow the + scheduled encounter with the asteroid 21-Lutetia and the rendezvous + with Churyumov-Gerasimenko. From an operational point of view, the + swing-by spacecraft operations were of highest priority, and both + science observations and payload operations were only allowed on a + non-interference basis with those. Keeping this in mind, Rosetta had + the opportunity to perform special scientific observations of the + Earth-Moon system, instrument calibrations using Earth and/or Moon + and public relations observations. + + The criticality of the spacecraft operations left payload operations + in a second place, provided that Earth is not a scientific target + for Rosetta and that potential trajectory correction manoeuvres + would force the cancellation of all of them. This is reflected in + the fact that only six instruments took part in the operations: + ALICE, MIRO, OSIRIS, RPC, VIRTIS and SREM. + Operation scheduling was centred on Earth Closest Approach, + which took place on 13 Nov. 2009 at 07:45:40 UTC, and overall + operations went smoothly, despite some scattered events. + According to the available reports, the EAR3 can be considered as + fully successful. + +EAR3 results are described in [RO-SGS-RP-0023]. + +Cruise phase 5 +-------------- +One Active checkout (12) was scheduled during this cruise phase. +It can be noted that Passive Checkout 11 were cancelled since there +was not enough time to include it between PC10 and PC12. PC 11 was +supposed to be passive meaning that it is mainly instrument +health check operations. PC 10 and 12 are active and more important to +preserve. + +Payload Checkout 12 (PC12) was an active checkout that ran for 23 +consecutive days starting on the 22nd April 2010 until the 14th May +2010. All Rosetta payload took part in this scenario. Operations +ranged from a repeat of established passive checkout operations to +extensive software patching and calibration campaigns. +Overall operations went smoothly. Numerous open issues were resolved +in this checkout, whilst several issues remain open and new ones have +been generated. There was a particularly noticeable and positive +increase in the success rate of payload operations, when compared to +previous Scenarios. + +All results can be read in [RO-SGS-RP-0027] report. + +Lutetia Flyby (17/05/2010 - 03/09/2010) +-------------- +The second of the flybys took place on 10 July 2010 to the asteroid +21 Lutetia, discovered on 15 November 1852 by H. Goldschmidt. Its +classification into a specific asteroid type had turned out to be +ambiguous and included the possibilities of a C-type or an M-type +asteroid. This contradiction made it an interesting object for close +inspection. +Closest Approach (CA) occurred at 15:45 UT at a distance of 3168.2km. +The relative fly-by velocity was of 15 km/s. The fly-by strategy +allowed continuous observations of Lutetia before, during and for 30 +minutes after CA. +Images obtained by OSIRIS revealed that Lutetia has a complex geology +and one of the highest asteroid densities measured so far, +3.4+/-0.3g/cm3. Its geologically complex surface, ancient surface age +and high density suggest that Lutetia is most likely a primordial +planetesimal. +This is the second of the two asteroids selected at the Science +Working Team meeting on 11th March 2004 among all the available +candidate asteroids, depending on the scientific interests and the +propellant required for the correction manoeuvre. + +The following operations took place around the Lutetia fly-by: +21 May 2010 - 9 July 2010: Navigation campaign (astrometry) using the +OSIRIS NAC and NAVCAM. +5 July 2010- 14 July 2010: scientific operations targeting the +asteroid. +The Lutetia fly-by was a success. The navigation campaign produced +highly accurate predictions of the position of Lutetia and during +the fly-by most instruments worked without serious problems (except +Rosina, RPC IES and RPC ICA). Asteroid fly-by mode worked excellently. +The objectives summarised below have been addressed by the instrument +measurements: + - Physical and thermal properties, mineralogy and geomorphology of + Lutetia from spatially resolved multi-wavelengths remote-sensing + observations between the extreme UV and the mm-range. + - Determination of the mass of the asteroid from Doppler + measurements of the spacecraft trajectory. + - Global shape parameters from light curves taken days before CA. + - Search for satellite/dust particles. + - Search for an asteroid magnetic field. + - Particle and field measurements. + +Results of the Lutetia Fly By can be found in [RO-SGS-RP-0028]. + +Rendez-Vous Manoeuver 1 (04/09/2010 - 13/07/2011) +---------------------- +The deep space manoeuvre was carried out when the spacecraft reached +a distance from the Sun around 4.5 AU on 23-Jan-11. One passive check +-out (13) was scheduled during this phase. One solar conjunction of +50 days and one solar opposition of 37 days happened during this +phase.(see Solar Conjunctions section above). + +--PC 13 (1st-9th Dec 2010 + 14th Dec) +This was the final Cruise Phase Checkout. A number of additional +payload operations were also executed, to close out pending and +essential requirements, and/or to configure instruments for the +upcoming Deep Space Hibernation Phase. Only OSIRIS did not participate +in PC 13. PC13 ran for 9 consecutive days between 1st and 9th December +2010. A RSI passive checkout was also completed on 14th December. +All of the operations planned and executed were successful. Minor +issues were observed by 4 instruments (Consert, Philae, Rosina, RPC). +Alice performed successfully some instrument checkout. +Cosima did periodical maintenance and check its status. +Giada checked successfully its status. +Midas performed a normal passive check-out and an additional modified +one for Deep Space Hibernation Preparation. +Miro performed a normal and successful passive check-out. +Osiris did not participate in the PC13 timeframe. However, on 23-26th +March 2011 - post RVM1 - specific OSIRIS operations were performed in +order to prepare and configure the instrument for the Rosetta Deep +Space Hibernation. +The Lander performed some operations and Consert performed an unit +functional test; both were partially successful. +Rosina did not participate in the nominal PC13 scenario, but conducted +several specific operations immediately following completion of the +nominal PC13 timeline. A spacecraft slew was executed with RTOF +monitoring, to further investigate data observed during Lutetia +fly-by. +RPC PIU, IES, LAP, ICA performed checkout with some errors/anomalies +reported, which were considered as no problem for the instrument. +Virtis performed the checkout successfully. +RSI measurements during PC13 showed some disturbances. The cause is +unknown at the time being. +SREM performed a successful checkout. + +More detailed results can be found in [RO-SGS-RP-0029]. + + +Cruise phase 6 (8 Jun 2011 - 20 Jan 2014) +-------------- +The whole period was spent in Deep-Space Hibernation Mode (DSHM). +Maximum distances to Sun and Earth are encountered during this +period, i.e. 5.3 AU (aphelion) and 6.3 AU, respectively. During this +phase, 3 superior solar conjunctions and 2 solar oppositions occurred +(see table above). This phase ended with the Spacecraft wake-up on +the 20th of January 2014. + +Rendez-Vous Manoeuver 2 (21 Jan 2014 - 9 Sep 2014) +---------------------- +The RVM2 started after Spacecraft wake-up and until September 2014, +when the Global Mapping phase started. It contained the Near Comet +Drift (NCD), the Far Approach Trajectory (FAT) and the Close Approach +Trajectory (CAT). It ended with the transition to Global Mapping. +During this phase, Rosetta did a series of ten OCMs, starting on the +7 May to reduce its speed with respect to comet 67P/C-G by about +775 m/s. The first, producing just 20 m/s delta-v ( change in +velocity ), was done as a small test burn, as it was the first use of +the spacecraft s propulsion system after wake-up. + +--Near comet drift (NCD) phase (21 May 2014 - 2 July 2014) + The following three OCMs form the Near Comet Drift (NCD) phase. + They took place every two weeks starting 21 May. They delivered + 289.6, 269.5 and 88.7 m/s in delta-v, respectively. + +-- Far Approach Trajectory (FAT) (2 July - 3 August 2014) + The FAT contained the next four burns. The four FAT burns was + carried out weekly during July, and all proceeded nominally. The + approach manoeuvre sequence reduced the relative velocity in stages + down to 3 m/s. + During this phase, the first images of the comet were obtained with + the optical measurement system (NAVCAM, OSIRIS). After detection, + knowledge of the comet ephemeris was drastically improved by + processing the on-board observations. Image processing on the ground + derived a coarse estimation of comet size, shape and rotation. + The first landmarks were identified. + + The FAT ends at the Approach Transition Point (ATP), which is + located in the Sun direction at about 1000 comet nucleus radii from + the nucleus. + + Find below a list of burns with delta-v reduction and duration + Date Delta-V m/s Dur.(mins) + 7 May 20 41 + 21 May 290 441 + 4 Jun 270 406 + 18 Jun 91 140 + 2 Jul 59 94 + 9 Jul 26 46 + 16 Jul 11 26 + 23 Jul 5 17 + 3 Aug 3 13 + 6 Aug 1 7 + +-- Close Approach Trajectory (CAT) + Close approach trajectory operations started at ATP. The spacecraft + distance to the comet was decreased to 20 nucleus radii and the + relative velocity fell below 1 m/s. The final point of this phase + was the Orbit Insertion Point (OIP), the point where the spacecraft + started orbiting the comet. + During the CAT, 5 landing sites were selected by the Landing team. + Details of the final manoeuvres to prepare insertion: + 6 August: Rosetta was commanded to conduct a 1-m/s thruster burn + (which ran 7 min) to change its direction and enter onto the first + arc (of three arcs) of two triangular (really, tetrahedral) orbits + about the comet. + It is important to note Rosetta has not been captured by 67P/C-G + gravity, and the continuing series of thruster burns were + necessary to keep the spacecraft at the comet. + + Rosetta executed two of these triangular orbits, one large, at + about 100km closest pass-by distance (Big CAT) and the second at + about 50km ( Little CAT ). + + 10 August: CAT Change 1 burn - a 6min:25sec, 0.88-m/s burn that + pushed Rosetta onto the next arc (100km pass-by height). + + 13 August: CAT Change 2 burn - a 6min:22sec, 0.87-m/s burn that + pushed Rosetta onto the next arc (100km pass-by height). + + 17 August: CAT Change 3 burn - a 6min:19sec, 0.85-m/s burn that + pushed Rosetta onto a transfer arc, down to about 80 km height + achieved on 20 Aug (CAT 4). + + Finally, with the next two burns on 24 and 27 August, the distance + was lowered to 50km. + + - Transition to Global Mapping (TGM) + On 31 August, Rosetta began the third and last arc of Little CAT + and Rosetta entered the TGM, a set of two manoeuvres. + The phase ended at 10 nucleus radii with ta relative velocity of + 0.3 m/s. + +Global Mapping and Close Observations (10 sep 2014 - 28 Oct 2014) +The Global Mapping phase ran 10 September to 15 October. During this +phase, Rosetta went down to 29 km distance, a point when the +spacecraft became actively captured by the comet gravity, and its +orbit became circular. + +At the beginning of this phase, the Lander team down selected 2 +landing sites: the nominal and the back up. + +A series of manoeuvres reduced Rosetta distance from 18.6 km orbit +(taking 7 days) to an intermediate orbit approximately 18.6 x 9.8 km +(with a period of 5 days). From there the orbit was circularised at +about 9.8 km radius, with a period of approximately 66 hours on 15 +October, and the mission entered the Close Observation Phase (COP). +This phase provided even higher resolution images of the landing +site in order to best prepare for Philae's challenging touch-down. +The new orbit also allowed a number of Rosetta's science instruments +to collect dust and measure the composition of gases closer to the +nucleus. + +On the 28 October, Rosetta conducted a thruster burn (82 sec from +12:59 UTC) that delivered a delta-v of 0.081 meters/sec. This pushed +the spacecraft to leave the 10-km-altitude circular orbit (following +the terminator line) and the COP. Rosetta started its transition to +the pre-lander-delivery orbit. +On 31 October, the mission control team performed another manoeuvre +to enter onto the pre-delivery orbit proper. + +Lander delivery +--------------- +On 31 October, Rosetta entered a pre-delivery elliptical orbit at +approximately 30 km distance from the comet centre. This orbit was +maintained until delivery on 12 November. +The orbiter performed its pre-separation manoeuvre at 6:04 on 12 +November, which placed it on the trajectory required for separation. +The separation occurred at 08:35 UTC (the confirmation signal arrived +on Earth at 09:03 UTC). At 10:34 UTC the Lander activated its +transmitters and started forwarding its telemetry to the orbiter. At +11:08 UTC, this telemetry was received on ground. +Touchdown was confirmed for Philae at 16:03 UTC. +While Lander telemetry kept flowing towards the Orbiter, the RF link +between the two crafts was regularly interrupted, which was not +consistent with a stable landing. Other Lander telemetry gave +indication that the Lander had bounced after initial touch-down. +The link between Orbiter and Lander was broken at 17:59 UTC one hour +earlier than expected for the targeted landing site. +On 13 November Lander telemetry was received on ground at 6:01 UTC, +very close to the expected time. + +During the descent, ROLIS acquired an image at 14:38:41 UT, from a +distance of approximately 3 km from the surface. The landing site was +imaged with a resolution of about 3m per pixel. + +After separation, Orbiter operations focus on maximising visibility +with the Lander and acquiring data to reconstruct the Lander descent +trajectory and support Orbiter Navigation. +NAVCAM and OSIRIS, once in Lander pointing, acquired every hour until +touch-down + 2 hours. After that, NAVCAM observed every 2 hours for +navigation. +The following Orbiter instruments have been operated: ALICE, CONSERT, +MIRO, OSIRIS, ROSINA, RPC. + +The post-delivery manoeuvre that has been executed on 12 November 2014 +started at 09:14:58.1 UTC and a nominal end time at 09:19:53.7 UTC. +Rosetta was then on a 50 km orbit. +On 13 November at 19:23 UTC Philae started transferring data to +Rosetta. Link was lost at 23:08 UTC on 13 November, 40 minutes before +predicted time. +During this slot was commanded: +- ranging measurements by CONSERT (Lander Search) +- CIVA images +- MUPUS boom deployment and hammering +- APXS deployment and measurement +On 14 November at 9:01, Philae data were received on-board Rosetta and +immediately transmitted to ground, 48 minutes after expected time. The +visibility period finished at 11:47 UTC on 14 November, 50 minutes +earlier than predicted. +During this period was commanded: +- APXS released but measured copper thus revealing that the door had + not opened. +- MUPUS deployment was successful, hammering took place, SESAME + detected it +- Drill activation for sample return to COSAC +- PTOLEMY/COSAC spectra acquisitions +- CIVA image but dark................................................. +- Consert ranging +The fourth and last Philae visibility period started on 14 November at +22:15 UTC ground time. The LAnder bus voltage appeared to decrease +rapidly. On November 15 at 00:07, the link between Orbiter and Lander +broke. +Among the Lander operations carried out during the fourth visibility +period was a rotation of the Lander to increase the illumination of +its solar arrays. + +After the planned Touch Down, the Lander did not anchor and bounced. +We estimated that the first TD was: + Time UTC: 15:34:06 + Comet-fixed coordinates: [2.129171, -0.961358, 0.498268] km +The NAVCAM image, the NAC image and the first TD as the starting point +gave the following impact point at: + Time UTC: 16:26:23 + Comet-fixed coordinates: [2.450, -0.511, -0.242] km +This point has an uncertainty of 7 minutes. The position is also +uncertain. +By using three WAC images, the second TD can be deduced: + Time UTC: 17:31:10 + Comet-fixed coordinates: [2.275, 0.249, -0.444] km +Consert Ranging estimated a final landing site at +Comet-fixed coordinates: [2.446, -0.055, -0.360] km + +After Touch Down, began the First Science Sequence (FSS) where all +Lander instruments operated on the primary battery. The operations +did not go as planned due to the several TDs but occurred as listed +above. The Long Term Science Phase should have started after the +primary battery died, but the final TD let the Lander in a location +where the illumination condition could not allow battery charging. +Contact was lost on 15 November 2014 at 00:07, ending the FSS, and the +Lander went asleep. + +Escort phase +------------ +Planning period during the comet phase were approximately monthly and +allowed changes in trajectory types every two weeks. The table below +summarises the trajectory followed by Rosetta after the Landing: +21 Nov - 3 Dec 2014 | Bound Orbits at 30 km +3 Dec - 6 Dec 2014 | Transition +6 Dec - 19 Dec 2014 | Bound Orbit at 20 km +19 Dec - 24 Dec 2014 | Transition +24 Dec - 4 Feb 2015 | Bound Orbit at 28 km +4 Feb - 21 Feb 2015 | Close FlyBy CA on 14 Feb at 8km + | Leg up to 143km +21 Feb - 10 Mar 2015 | Arcs around 80 km +Apr 2015 | Fly bys: CA of 90 km and maximum distance + | of 180km +May 2015 | Fly bys: first from 125km to 180 km then from + | 200km to 325km +June 2015 | Fly bys: from 200 to 240km then CA to 160km + | Sub s/c point located North for Lander com. +July 2015 | Fly bys: CA at 150 km +Aug 2015 | Fly bys: CA increased to 180 km (star tracker + | issues. +Sept 2015 | Fly bys: between 400 and 460km first then + | reduced to 300-330 km +Oct 2015 | Far excursion at 1500 km +Nov 2015 | Fly bys from 420 to 140km +Dec 2015 | Fly bys (75-150km) +Jan 2016 | Fly bys (45-95km) +Feb 2016 | Fly bys (32-52km) +Mar 2016 | Terminator orbit (17 to 12km) - night side + | excursion - far excursion at 1000km - + | hyperbolic arcs at 200km +Apr 2016 | Far Flyby arcs at 200km in terminator - Flyby + | arcs at 80 km at 80 deg - Close Flyby at 30km + | Outbound arc (140 to 70km) at terminator - + | insertion into bound orbits at 19km dist. +May 2016 | Bound orbits in terminator plane: first + | elliptical 19kmx10km - circular 10km - + | circular 7km - mapping orbit at 17km. +Jun 2016 | Mapping orbit at 17km - at 30 km - 2 day-side + | half orbit at 45 deg phase angle - elliptical + | 28x14km at terminator +Jul 2016 | 2.5 elliptical orbit 26x9km at terminator - + | circular orbit at 10 km at terminator +26 Jul - 9 Aug 2016 | 4 elliptical orbits 14x8km with 70-110 deg + | phase angles +9 Aug - 2 Sep 2016 | elliptical orbits (70-110 deg phase angles). + | Pericentre gradually reduced and apocentre + | increased while constant orbital period of 3 + | days 13.7km, 7.5km, 13.7km, 6.7km, 14.4km, + | 6.0km, 15.1km, 5.5km, 15.5km, 5.0km, 15.9km, + | 4.6km, 16.2km, 4.4km, 16.4km +2 Sep - 26 Sep 2016 | elliptical orbits (70-110 deg phase angles). + | Pericentre gradually reduced and apocentre + | increased while constant orbital period of 3 + | days 4.0km, 17.1km, 3.9km, 17.1km, 4.1km, + | 16.1km, 4.1km, 16.8km, 4.1km, 16.0km, 4.1km, + | 17.0km, 4.1km, 16.7km, 4.1km, 17.2km +26 Sep - 30 Sep 2016 | exit from elliptical orbits - hyperbolic arcs + | with dist from 17 to 23km - final descent to + | the comet nucleus. + +Orbiter Experiments +===================================================================== + +ALICE +----- +ALICE, an Ultraviolet Imaging Spectrometer, characterise the +composition of the nucleus and coma, and the nucleus/coma coupling of +comet 67 P/Churyumov-Gerasimenko. This is accomplished through the +observation of spectral features in the extreme and far ultraviolet +(EUV/FUV) spectral regions from 70 to 205 nm. + +ALICE make measurements of noble gas abundances in the coma, the +atomic budget in the coma, and major ion abundances in the tail and +in the region where solar wind particles interact with the ionosphere +of the comet. ALICE determine the production rates, variability, +and structure of H2O and CO, and CO2 gas surrounding the nucleus and +the far-UV properties of solid grains in the coma. + +ALICE studied Mars and the Rosetta asteroid flyby targets while en +route to Churyumov- Gerasimenko. ALICE also map the cometary nucleus +in the FUV + +Instrument References: [STERNETAL2007] + +CONSERT +------- +CONSERT (Comet Nucleus Sounding Experiment by Radio wave +Transmission) is an experiment that perform tomography of the +comet nucleus revealing its internal structure. CONSERT operates as a +time domain transponder between the Lander on the comet surface and +the Orbiter. A radio signal passes from the orbiting component of the +instrument to the component on the comet surface and is then +immediately transmitted back to its source, the idea being to +establish a radio link that passes through the comet nucleus. The +varying propagation delay as the radio waves pass through different +parts of the cometary nucleus is used to determine the dielectric +properties of the nuclear material. Many properties of the comet +nucleus is examined as its overall structural homogeneity, the average + size of the sub-structures (Cometesimals) and the number and + thickness of the various layers beneath the surface. + +Instrument References: [KOFMANETAL2007] + +COSIMA +------ +The Cometary Secondary Ion Mass Analyser is a secondary ion mass +spectrometer equipped with a dust collector, a primary ion gun, and +an optical microscope for target characterization. Dust from the near +comet environment is collected on a target. The target is then moved +under a microscope where the positions of any dust particles are +determined. The cometary dust particles are then bombarded with pulses +of indium ions from the primary ion gun. The resulting secondary ions +are extracted into the time-of-flight mass spectrometer. + +Instrument References: [KISSELETAL2007] + +GIADA +----- +The Grain Impact Analyser and Dust Accumulator measures the +scalar velocity, size and momentum of dust particles in the coma of +the comet using an optical grain detection system and a mechanical +grain impact sensor. Five microbalances measure the amount of +dust collected as the spacecraft orbits the comet. + +Instrument References: [COLANGELIETAL2007] + +MIDAS +----- +The Micro-Imaging Dust Analysis System is intended for the +microtextural and statistical analysis of cometary dust particles. +The instrument is based on the technique of atomic force microscopy. +This technique, under the conditions prevailing at the Rosetta +Orbiter permits textural and other analysis of dust particles to be +performed down to a spatial resolution of 4nm. + +Instrument References: [RIEDLERETAL2007] + +MIRO +---- +MIRO (Microwave Instrument for the Rosetta Orbiter) is composed of a +millimetre wave mixer receiver and a submillimetre heterodyne +receiver. The submillimetre wave receiver provides both broad band +continuum and high resolution spectroscopic data, whereas the +millimetre wave receiver provides continuum data only. + +MIRO measures the near surface temperature of the comet, allowing +estimation of the thermal and electrical properties of the surface. +In addition, the spectrometer portion of MIRO allows measurements +of water, carbon monoxide, ammonia, and methanol in the comet coma. + +Instrument References: [GULKISETAL2007] + +OSIRIS +------ +OSIRIS (Optical, Spectroscopic, and Infrared Remote Imaging System) +is a dual camera imaging system operating in the visible, near +infrared and near ultraviolet wavelength ranges. OSIRIS consists of +two independent camera systems sharing common electronics. The narrow +angle camera is designed to produce high spatial resolution images of +the nucleus of the target comet. The wide angle camera has a wide +field of view and high straylight rejection to image the dust and gas +directly above the surface of the nucleus of the target comet. Each +camera is equipped with filter wheels to allow selection of imaging +wavelengths for various purposes. The spectroscopic and wider band +infrared imaging capabilities originally proposed and incorporated in +the instrument name were descoped during development. + +Instrument References: [KELLERETAL2006] + +ROSINA +------ +ROSINA (Rosetta Orbiter Spectrometer for Ion and Neutral Analysis) +consists of two mass spectrometers, since no one technique is able to +achieve the resolution and accuracy required to fulfil the ROSETTA +mission goals over the range of molecular masses under analysis. In +addition, two pressure gauges provide density and velocity data for +the cometary gas. + +The two mass analysers are: +* A double focusing magnetic mass spectrometer with a mass range of 1 +- 100 amu and a mass resolution of 3000 at 1 % peak height, optimised +for very high mass resolution and large dynamic range +* A reflectron type time-of-flight mass spectrometer with a mass +range of 1 -300 amu and a mass resolution better than 500 at 1 % peak +height, optimised for high sensitivity over a very broad mass range + +Instrument References: [BALSIGERETAL2007] + +RPC +--- +RPC (Rosetta Plasma Consortium) is a set of five sensors sharing a +common electrical and data interface with the Rosetta orbiter. The +RPC sensors are designed to make complementary measurements of the +plasma environment around the comet 67P/Churyumov-Gerasimenko. + +The RPC sensors are: +* ICA: an Ion Composition Analyser, which measures the three- + dimensional velocity distribution and mass distribution of positive + ions; +* IES: an Ion and Electron Sensor, which simultaneously measures + the flux of electrons and ions in the plasma surrounding the comet; +* LAP: a Langmuir Probe, which measures the density, temperature + and flow velocity of the cometary plasma; +* MAG: a Fluxgate Magnetometer, which measures the magnetic field + in the region where the solar wind plasma interacts with the comet; + Instrument References: [GLASSMEIERETAL2007B] +* MIP: a Mutual Impedance Probe, which derives the electron plasma + density, and can sometimes constrain other plasma parameters of the inner + coma of the comet. + +Instrument References: [CARRETAL2007] + +RSI +--- +RSI (Radio Science Investigation) makes use of the communication +system that the Rosetta spacecraft uses to communicate with the +ground stations on Earth. Either one-way or two-way radio links can +be used for the investigations. In the one-way case, a signal +generated by an ultra-stable oscillator on the spacecraft is received +on earth for analysis. In the two way case, a signal transmitted from +the ground station is transmitted back to Earth by the spacecraft. In +either case, the downlink may be performed in either X-band or both X +-band and S-band. + +RSI investigates the nondispersive frequency shifts (classical +Doppler) and dispersive frequency shifts (due to the ionised +propagation medium), the signal power and the polarization of the +radio carrier waves. Variations in these parameters yields +information on the motion of the spacecraft, the perturbing forces +acting on the spacecraft and the propagation medium. + +Instrument References: [PAETZOLDETAL2007] + +VIRTIS +------ +VIRTIS (Visible and Infrared Thermal Imaging Spectrometer) is an +imaging spectrometer that combines three data channels in one +instrument. Two of the data channels are committed to spectral +mapping and are housed in the Mapper optical subsystem. The third +channel is devoted solely to spectroscopy and is housed in the High +resolution optical subsystem. + +The mapping channel optical system is a Shafer telescope consisting +of five aluminium mirrors mounted on an aluminium optical bench. The +mapping channel uses a silicon charge coupled device (CCD) to detect +wavelengths from 0.25 micron to 1 micron and a mercury cadmium +telluride (HgCdTe) infrared focal plane array (IRFPA) to detect from +0.95 micron to 5 microns. + +The high resolution channel is an echelle spectrometer. The incident +light is collected by an off-axis parabolic mirror and then +collimated by another off-axis parabola before entering a cross- +dispersion prism. After exiting the prism, the light is diffracted by +a flat reflection grating, which disperses the light in a direction +perpendicular to the prism dispersion. The high-resolution channel +employs a HgCdTe IRFPA to perform detection from 2 to 5 microns. + +Instrument References: [CORADINIETAL2007] + +SREM +---- +The Standard Radiation Environment Monitor (SREM) is a monitor-class +instrument intended for space radiation environment characterisation +and radiation housekeeping purposes. SREM provides continuous +directional, temporal, and spectral data of high-energy electron, +proton, and cosmic ray fluxes encountered along the orbit of the +spacecraft, as well as measurements of the total accumulated +radiation dose absorbed by SREM itself. + +This instrument is a facility monitor flown on several ESA +spacecrafts. It is not considered as a PI (Principal Investigator) +instrument. + +Instrument References: [MOHAMMADZADEETAL2003] + + +LANDER (PHILAE) +===================================================================== + +The 100 kg Rosetta Lander, named Philae, is the first spacecraft +ever to make a soft landing on the surface of a comet nucleus. The +Lander is provided by a European consortium under the leadership of +the German Aerospace Research Institute (DLR) and the French Space +Research Center (CNES). Other members of the consortium are ESA and +institutes from Austria, Finland, France, Hungary, Ireland, Italy and +the UK. A description of the Lander can be found in [RO-EST-RS-3020]. + +The box-shaped Lander was carried in piggyback fashion on the side of +the Orbiter until it arrived at Comet 67P/Churyumov-Gerasimenko. Once +the Orbiter was aligned correctly, the ground station commanded the +Lander to self-eject from the main spacecraft and unfold its three +legs, ready for a gentle touch down at the end of the ballistic +descent. The Landing is described above. + +Immediately after touchdown, a harpoon was supposed to fire to anchor +the Lander to the ground and prevent it escaping from the comet's +extremely weak gravity. The system did not work and the Lander bounced +several times. + +Science Objectives +------------------ +It is the general aim of the scientific experiments carried and +operated by the Rosetta Lander to obtain a first in situ composition +analysis of primitive material from the early solar system, to study +the composition and structure of a cometary nucleus, reflecting +growth processes in the early solar system, to provide ground truth +data for the Rosetta Orbiter experiments and to investigate dynamic +processes leading to changes in cometary activity. + +The primary objective of the Rosetta Lander mission is the in situ +investigation of the elemental, isotopic, molecular and mineralogic +composition and the morphology of early solar system material as it +is preserved in the cometary nucleus. Measurement of the absorption +and phase shift of electromagnetic waves penetrating the comet +nucleus will help to determine its internal structure. Seismometry +and magnetometry will also be used to investigate the interior of the +comet. + +The scientific objectives of the Rosetta Lander can be listed +according to their priority as follows: +1. Determination of the composition of cometary surface and + subsurface matter: bulk elemental abundances, isotopic ratios, + minerals, ices, carbonaceous compounds, organics, volatiles - also + in dependence on time and insolation. +2. Investigation of the structure and physical properties of the + cometary surface: topography, texture, roughness, regolith scales, + mechanical, electrical, optical, and thermal properties, + temperatures. Characterization of the near surface plasma + environment. +3. Investigation of the global internal structure. +4. Investigation of the comet/plasma interaction. + +The in situ measurements performed by the Rosetta Lander instruments +will also provide local ground truth to calibrate Orbiter +instruments. + +Lander Experiments +------------------ + +Here a description of all the instruments of the Lander: + +APXS: Alpha-p-X-ray spectrometer +- - - - - - - - - - - - - - - - +The goal of the Rosetta APXS experiment is the determination of the +chemical composition of the landing site and its potential alteration +during the comet's approach to the Sun. The data obtained is +used to characterize the surface of the comet, to determine the +chemical composition of the dust component, and to compare the dust +with known meteorite types. + +Instrument References: [KLINGELHOFERETAL2007] + +CIVA: Panoramic and microscopic imaging system +- - - - - - - - - - - - - - - - - - - - - - - - +The Cometary Infrared and Visible Analiser (CIVA) is an integrated +set of imaging instruments, designed to characterize the landing and +sampling site, the 360 deg panorama as seen from the Rosetta Lander, +all samples collected and delivered by the Drill Sample and +Distribution System, and the stratigraphy within the boreholes. It is +constituted by a panoramic stereo camera (CIVA-P), and a microscope +coupled to an IR spectrometer (CIVA-M). CIVA is sharing a common +Imaging Main Electronics (CIVA/ROLIS/IME) with ROLIS. CIVA-P will +characterize the landing site, from the landing legs to the local +horizon. The camera is composed of 6 identical micro-cameras, mounted +of the Lander sides, with their optical axes separated by 60 deg. In +addition, stereoscopic capability is provided by one additional micro- +camera, identical to and co-aligned with one of the panoramic micro- +camera, with its optical axis 10 cm apart. + +CIVA-M combines in separated boxes, two ultra-compact and +miniaturized channels, one visible microscope CIVA-M/V and one IR +spectrometer CIVA-M/I, to characterize, by non-destructive analyses, +the texture, albedo, mineralogical and molecular composition of each +of the samples collected and distributed by the Drill Sample and +Distribution System. + +Instrument References: [BIBRINGETAL2007A] + +CONSERT: Radio sounding, nucleus tomography +- - - - - - - - - - - - - - - - - - - - - - +The Comet Nucleus Sounding Experiment by Radio wave Transmission +(CONSERT) is a complex experiment that performs tomography of the +comet nucleus revealing its internal structure. CONSERT operates as a +time domain transponder between the Lander, on the comet surface and +the Orbiter orbiting the comet. A radio signal passes from the +orbiting component of the instrument to the component on the comet +surface and is then immediately transmitted back to its source, the +idea being to establish a radio link that passes through the comet +nucleus. The varying propagation delay as the radio waves pass through +different parts of the cometary nucleus is used to determine the +dielectric properties of the nuclear material. Many properties of the +comet nucleus is examined as its overall structural homogeneity, the +average size of the sub-structures (Cometesimals) and the number and +thickness of the various layers beneath the surface. + +Instrument References: [KOFMANETAL2007] + +COSAC: Evolved gas analyser - elemental and molecular composition +- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - +The COmetary SAmpling and Composition experiment COSAC is one of the +two 'evolved gas analysers' (EGAs) on board the Rosetta-Lander. +Whereas the other EGA, Ptolemy, aims mainly at accurately measuring +isotopic ratios of light elements, the COSAC is specialised on +detection and identification of complex organic molecules. The +instrument can be described as an effort to analyse in situ, mainly +with respect to the composition of the volatile fraction, cometary +matter nearly as well and accurately as could be done in a laboratory +on Earth. Due to the Rosetta Lander rotatability, the instrument can +conduct analyses and investigations at different spots of the landing +site and, aided by the drill, take samples for analysis from a depth +up to at least 0.2 m. +Instrument References: [GOESMANNETAL2007] + +PTOLEMY: Evolved gas analyser - isotopic composition +- - - - - - - - - - - - - - - - - - - - - - - - - - - +The size of a small shoe box and weighing less than 5 kg, Ptolemy +uses gas chromatography / mass spectrometry (GCMS) techniques to +investigate the comet surface & subsurface. The instrument concept is +termed 'MODULUS' which is taken to mean Methods Of Determining and +Understanding Light elements from Unequivocal Stable isotope +compositions. The scientific goal of the PTOLEMY is to understand the +geochemistry of light elements, such as hydrogen, carbon, nitrogen +and oxygen, by determining their nature, distribution and stable +isotopic compositions. +Instrument References: [WRIGHTETAL2007] + +MUPUS: Measurements of surface and subsurface properties +- - - - - - - - - - - - - - - - - - - - - - - - - - - - - +The Multi-Purpose Sensor Experiment actually consists of four parts: +1. A penetrator, approximately 40 cm long, is hammered into the +ground about 1m apart from the Lander for measuring during the +penetration process the mechanical strength of the material by means +of a depth sensor and a densitometer. The penetrator is equipped with +a series of temperature sensors and heaters for determining the +temperature as a function of depth and insolation. +2. An accelerometer and a temperature sensor accommodated in the +harpoon(s) +3. A four-channel infrared radiometer measures surface temperatures +in the vicinity of the Lander. Density of the nearsurface (down to +20cm) material is determined by measuring the absorption of +gamma-rays emitted from a radioactive isotope mounted at the tip of +the penetrator. +Instrument References: [SPOHNETAL2007] + +ROLIS: Descent & Down-Looking Imaging +- - - - - - - - - - - - - - - - - - - +The ROLIS Camera (Rosetta Lander Imaging System) delivered first +close-ups of the environment of the landing place of comet +67P/Churyumov-Gerasimenko during the descent. +After landing ROLIS made high-resolved investigations to study +the structure (morphology) and mineralogy of the surface. +Instrument References: [MOTTOLAETAL2007] + +ROMAP: Magnetometer and plasma monitor +- - - - - - - - - - - - - - - - - - - - +The Rosetta Lander Magnetometer and Plasma Monitor ROMAP is a multi- +sensor experiment. The magnetic field is measured with a fluxgate +magnetometer. An electrostatic analyzer with integrated Faraday cup +measures ions and electrons. The local pressure is measured with +Pirani and Penning sensors. The sensors are situated on a short boom. +The deployment on the surface of a cometary nucleus demanded the +development of a special digital magnetometer of little weight and +small power requirements. For the first time a magnetic sensor is +operated from within a plasma sensor. A prototype of the +magnetometer, named SPRUTMAG, was flown on space station MIR. +Instrument References: [AUSTERETAL2007] + +SD2: Sampling, Drilling and Distribution Subsystem +- - - - - - - - - - - - - - - - - - - - - - - - - - +The Rosetta-Lander is equipped with a Sample Drill & Distribution +(SD2) subsystem which is in charge to collect cometary surface +samples at given depth and distribute them to the following +instruments: CIVA-M (microscope (MS) & Infrared Spectrometer (IS)), +the ovens, serving COSAC and PTOLEMY. + +Comet sample from pre-determined and/or known (measured) depth are +collected and transported by SD2 to well defined locations: +* MS & IS viewing place +* ovens for high temperature (800 deg C) heating +* ovens for medium temperature (130 deg C) heating. +* ovens with a window, where samples can be investigated by CIVA-M +The sampling, drilling and distribution (SD2) subsystem provides +microscopes and advanced gas analysers with samples collected at +different depths below the surface of the comet. Specifically SD2 can +bore up to 250 mm into the surface of the comet and collect samples +of material at predetermined and/or known depths. It then transports +each sample to a carousel which feeds samples to different instrument +stations: a spectrometer, a volume check plug, ovens for high and +medium temperatures and a cleaning station. SD2 is accommodated +on the flat ground-plate of the Rosetta, where it is exposed to +the cometary environment. +Instrument References: [ERCOLIFINZIETAL2007] + +SESAME: Surface electrical, acoustic and dust impact monitoring +- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - +The SESAME (Surface Electrical, Seismic and Acoustic Monitoring +Experiments) electronics board and the integration of the components +are managed by the German Aerospace Center (DLR), Institute of Space +Simulation, Cologne. + +The results of SESAME help in understanding how comets, have +formed and thus, how the solar system, including the Earth, was born. +Instrument References: [SEIDENSTICKERETA2007] + + +GROUND SEGMENT +===================================================================== + +This section summarizes the roles and responsibilities for the +Rosetta Ground Segment. + +The primary responsibility for developing the payload operations +strategy for the Rosetta Scientific Mission is the Rosetta Science +Working Team. The Rosetta Science Working Team (SWT) monitors and +advises on all aspects of Rosetta which affect its scientific +performance. + +Rosetta Ground Segment +----------------------- +The Rosetta ground segment consists of two major elements: the +Rosetta Mission Operations Centre (RMOC) and the Rosetta Science +Ground Segment (RSGS). + +Rosetta Science Ground Segment +- - - - - - - - - - - - - - - - - - +The Rosetta Science Ground Segment (RSGS) is located at the +European Space Astronomy Centre (ESAC) in Spain. The main task is to +support the Rosetta Project Scientist in the planning of the science +operations schedule and in the generation of coordinated operational +sequences, the payload command sequences for all Rosetta instruments +and their onward transmission to the Rosetta Mission Operations Centre +(RMOC). In addition, the RSGS prepares the trajectory during the comet +escort phase. + +Rosetta Mission Operations Center +- - - - - - - - - - - - - - - - - - +The Rosetta Mission Operations Center (RMOC) is located at the +European Space Operations Center (ESOC) in Darmstadt, Germany. The +RMOC is responsible for the Spacecraft operations and all real time +contacts with the spacecraft and payload, the overall mission +planning, flight dynamics and spacecraft and payload data +distribution. + +Rosetta Lander Ground Segment +------------------------------ +The Rosetta Lander Ground Segment (RLGS) is made up of two +operational teams. When CNES joined the DLR consortium for developing +the Lander, it was decided to divide the RLGS into 2 centers (see +Lander Project Plan [RL-PL-DLR-97002]). +These teams are responsible for the success of the Lander operations, +to ensure that the Lander performs the science with regards to its +status, and to give the data to the PI's and suppliers. + +Lander Control Center +- - - - - - - - - - - - +The Lander Control Center (LCC), located at DLR/MUSC in Koeln +(Germany), in charge of Rosetta Lander operations during the flight +segment definition, design, realization, assembly and tests. + +Science Operations and Navigation Center +- - - - - - - - - - - - - - - - - - - - - +The Science Operations and Navigation Center is under CNES +responsibility, located in Toulouse (France). It is responsible for +the navigation and mission analysis aspects, including separation, +landing and descent strategies and generation of the scientific +sequences. + +Rosetta Scientific Data Archive +-------------------------------- +All scientific data obtained during the full mission duration +remains proprietary of the PI teams and the Lander teams for a maximum +period of 6 months after they have been received from ESOC. After +this period, the scientific data products from the mission have to be +submitted to RSOC in a reduced and calibrated form such that they can +be used by the scientific community. The Archive Scientist prepares +the release of Rosetta Scientific Data Archive after reception from +the individual Rosetta instruments and after the 6 months proprietary +period. + + +Acronyms +-------- +For more acronyms refer to Rosetta Project Glossary [RO-EST-LI-5012] + +ATTC Absolute Time Telecommand +AU Astronomical Unit +CA Closest Approach +CAP Comet Acquisition Point +CAT Close Approach Trajectory +CNES Centre National d'Etudes Spatiales +COP Close Observation Phase +DLR German Aerospace Center +DSM Deep Space Manoeuver +ESA European Space Agency +ESAC European Space Astronomy Centre +ESOC European Space Operations Center +ESTEC European Space Research and Technology Center +EUV Extreme UltraViolet +FAT Far approach trajectory +FSS First Science Sequence +FUV Far UltraViolet +GCMS Gas Chromatography / Mass Spectrometry +GMP Global Mapping Phase +HGA High Gain Antenna +HgCdTe Mercury Cadmium Telluride +HIGH High Activity Phase (Escort Phase) +HK HouseKeeping +IRAS InfraRed Astronomical Satellite +IRFPA Infrared Focal Plane Array +IS Infrared Spectrometer +LCC Lander Control Center +LDL Long Debye Length +LEOP Launch and Early Orbit Phase +LOW Low Activity Phase (Escort Phase) +LTE Local Thermodynamic Equilibrium +MINC Moderate Increase Phase (Escort Phase) +MGA Medium Gain Antenna +MLI Multi Layer Insulation +MS Microscope +NNO New Norcia ground station +OCM Orbit Correction Manoeuvres +OIP Orbit Insertion Point +PI Principal Investigator +P/L PayLoad +PC Payload Checkout +PDHC Pre Delivery Calib Science +PHC Post Hibernation Commissioning +PRL Prelanding +RBD Rebounds +RF Radio Frequency +RMOC Rosetta Mission Operations Center +RLGS Rosetta Lander Ground Segment +RL Rosetta Lander +RO Rosetta Orbiter +RSGS Rosetta Science Ground Segment +RVM Rendez-vous Manoeuver +S/C SpaceCraft +SDL Separation Descent and Landing +SINC Sharp Increase Phase (Escort Phase) +SONC Science Operations and Navigation Center +SSP Surface Science Package +STR Star TRacker +SWT Science Working Team +TGM Transition to global mapping + +" + + END_OBJECT = MISSION_INFORMATION + + /* Two MISSION_HOST objects, one for each Inst_host. */ + /* See PDS Standard B.24 */ + + OBJECT = MISSION_HOST + INSTRUMENT_HOST_ID = RO + + OBJECT = MISSION_TARGET + TARGET_NAME = "67P/CHURYUMOV-GERASIMENKO 1 (1969 R1)" + END_OBJECT = MISSION_TARGET + + OBJECT = MISSION_TARGET + TARGET_NAME = "2867 STEINS" + END_OBJECT = MISSION_TARGET + + OBJECT = MISSION_TARGET + TARGET_NAME = "21 LUTETIA" + END_OBJECT = MISSION_TARGET + + OBJECT = MISSION_TARGET + TARGET_NAME = "EARTH" + END_OBJECT = MISSION_TARGET + + OBJECT = MISSION_TARGET + TARGET_NAME = "MARS" + END_OBJECT = MISSION_TARGET + + OBJECT = MISSION_TARGET + TARGET_NAME = "9P/TEMPEL 1 (1867 G1)" + END_OBJECT = MISSION_TARGET + + END_OBJECT = MISSION_HOST + + OBJECT = MISSION_HOST + INSTRUMENT_HOST_ID = RL + + OBJECT = MISSION_TARGET + TARGET_NAME = "67P/CHURYUMOV-GERASIMENKO 1 (1969 R1)" + END_OBJECT = MISSION_TARGET + + END_OBJECT = MISSION_HOST + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "RL-PL-DLR-97002" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "RO-DSS-MA-1001" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "RO-ESC-PL-5000" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "RO-ESC-PL-5026" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "RO-EST-AO-0001" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "RO-EST-LI-5012" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "RO-EST-PL-2010" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "RO-EST-RP-3293" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "RO-EST-RP-3307" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "RO-EST-RP-3318" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "RO-EST-RP-3321" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "RO-EST-RP-3341" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "RO-EST-RP-3342" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "RO-EST-RP-3343" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "RO-EST-RP-3418" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "RO-EST-RP-3464" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "RO-EST-RS-3020" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "RO-SGS-RP-0001" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "RO-SGS-RP-0002" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "RO-SGS-RP-0004" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "RO-SGS-RP-0005" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "RO-SGS-RP-0019" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "RO-SGS-RP-0020" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "RO-SGS-RP-0022" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "RO-SGS-RP-0023" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "RO-SGS-RP-0027" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "RO-SGS-RP-0028" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "RO-SGS-RP-0029" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "RO-SGS-RP-0030" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "AUSTERETAL2007" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "BALSIGERETAL2007" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "BIBRINGETAL2007A" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "CARRETAL2007" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "COLANGELIETAL2007" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "CORADINIETAL2007" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "ERCOLIFINZIETAL2007" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "GLASSMEIERETAL2007A" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "GLASSMEIERETAL2007B" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "GOESMANNETAL2007" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "GULKISETAL2007" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "KELLERETAL2006" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "KELLERETAL2010" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "KISSELETAL2007" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "KLINGELHOFERETAL2007" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "KOFMANETAL2007" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "LAMYETAL2008" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "MOHAMMADZADEETAL2003" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "MOTTOLAETAL2007" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "PAETZOLDETAL2007" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "RIEDLERETAL2007" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "SEIDENSTICKERETA2007" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "SPOHNETAL2007" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "STERNETAL2007" + END_OBJECT = MISSION_REFERENCE_INFORMATION + + OBJECT = MISSION_REFERENCE_INFORMATION + REFERENCE_KEY_ID = "WRIGHTETAL2007" + END_OBJECT = MISSION_REFERENCE_INFORMATION + +END_OBJECT = MISSION + +END diff --git a/data/pds4/context_support/document/collection.xml b/data/pds4/context_support/document/collection.xml new file mode 100644 index 00000000..4bc80c2b --- /dev/null +++ b/data/pds4/context_support/document/collection.xml @@ -0,0 +1,65 @@ + + + + + + urn:nasa:pds:context_support:document + 1.0 + Context Product Supporting Documents + 1.22.0.0 + Product_Collection + + 2024 + + The collection contains documents to support context products for + legacy data sets not yet migrated to PDS4 status (and thus with + no documents that can be referenced by LIDs). It also contains + documents created by extracting extended DESCRIPTION fields from + PDS3 catalog files. + + + + + 2024-08-01 + 1.0 + + Creation + + + + + + Document + + + + inventory.csv + + + 0 + PDS DSV 1 + 9 + Carriage-Return Line-Feed + Comma + + 2 + 0 + + Member Status + 1 + ASCII_String + 1 + + + LIDVID_LID + 2 + ASCII_LIDVID_LID + 255 + + + inventory_has_member_product + + + \ No newline at end of file diff --git a/data/pds4/context_support/document/description/catalinaSkySurvey.docx b/data/pds4/context_support/document/description/catalinaSkySurvey.docx new file mode 100644 index 00000000..26830260 Binary files /dev/null and b/data/pds4/context_support/document/description/catalinaSkySurvey.docx differ diff --git a/data/pds4/context_support/document/description/catalinaSkySurvey.xml b/data/pds4/context_support/document/description/catalinaSkySurvey.xml new file mode 100644 index 00000000..887a1c36 --- /dev/null +++ b/data/pds4/context_support/document/description/catalinaSkySurvey.xml @@ -0,0 +1,45 @@ + + + + + + urn:nasa:pds:context_support:document:css_description + 1.0 + Catalina Sky Survey Description + 1.22.0.0 + Product_Document + + + 2024 + + Description of the Catalina Sky Survey extracted from the investigation + context product for that survey. + + + + + + 2024-07-31 + 1.0 + + Creation from existing, unattributed text. + + + + + + + 2024-08 + + MS Word + English + 1 + + catalinaSkySurvey.docx + Microsoft Word + + + + \ No newline at end of file diff --git a/data/pds4/context_support/document/description/cometNucleusTour.docx b/data/pds4/context_support/document/description/cometNucleusTour.docx new file mode 100644 index 00000000..32c72608 Binary files /dev/null and b/data/pds4/context_support/document/description/cometNucleusTour.docx differ diff --git a/data/pds4/context_support/document/description/cometNucleusTour.xml b/data/pds4/context_support/document/description/cometNucleusTour.xml new file mode 100644 index 00000000..295207bc --- /dev/null +++ b/data/pds4/context_support/document/description/cometNucleusTour.xml @@ -0,0 +1,44 @@ + + + + + + + urn:nasa:pds:context_support:document:contour_description + 1.0 + Comet Nucleus Tour Description + 1.22.0.0 + Product_Document + + 2024 + + Brief description of the Comet Nucleus Tour (CONTOUR) mission + quoted from a website available in 2016 and used by permission + of NASA. + + + + + 2024-08-01 + 1.0 + + Creation + + + + + + 2016-10 + + MSWord + English + 1 + + cometNucleusTour.docx + Microsoft Word + + + + \ No newline at end of file diff --git a/data/pds4/context_support/document/description/dawn.docx b/data/pds4/context_support/document/description/dawn.docx new file mode 100644 index 00000000..28a7606e Binary files /dev/null and b/data/pds4/context_support/document/description/dawn.docx differ diff --git a/data/pds4/context_support/document/description/dawn.xml b/data/pds4/context_support/document/description/dawn.xml new file mode 100644 index 00000000..d9f7b7c2 --- /dev/null +++ b/data/pds4/context_support/document/description/dawn.xml @@ -0,0 +1,45 @@ + + + + + + urn:nasa:pds:context_support:document:dawn_description + 1.0 + Dawn Description + 1.22.0.0 + Product_Document + + 2024 + + The document contains an unattributed description of the Dawn mission + extracted from the PDS3 mission catalog file DESCRIPTION keyword. It + includes mission/science goals, brief descriptions of instruments and + mission phases, and a mission phase table that has been updated with + the date at which contact was lost with the spacecraft. + + + + + 2024-08-01 + 1.0 + + Creation + + + + + + 2016 + + MSWord + English + 1 + + dawn.docx + Microsoft Word + + + + \ No newline at end of file diff --git a/data/pds4/context_support/document/description/deepImpact.docx b/data/pds4/context_support/document/description/deepImpact.docx new file mode 100644 index 00000000..dffcd255 Binary files /dev/null and b/data/pds4/context_support/document/description/deepImpact.docx differ diff --git a/data/pds4/context_support/document/description/deepImpact.xml b/data/pds4/context_support/document/description/deepImpact.xml new file mode 100644 index 00000000..baa36e0c --- /dev/null +++ b/data/pds4/context_support/document/description/deepImpact.xml @@ -0,0 +1,54 @@ + + + + + + urn:nasa:pds:context_support:document:di_description + 1.0 + Deep Impact Description + 1.22.0.0 + Product_Document + + 2024 + + This document was extracted from the description section of the + PDS3 mission catalog file, augmented with the (decoded) reference + list from that file, and put into MS Word format for ease of + reading. Minor typos were corrected, HTML character entities were + replaced with the corresponding character, and PDS3 REFERENCE_KEY_ID + values, which duplicated inline citations, were removed. + + + + Anne + Raugh + https://orcid.org/0000-0002-8300-9443 + + + + + + 2024-08-01 + 1.0 + + Creation + + + + + + + 2024-08 + + MSWord + English + 1 + + deepImpact.docx + Microsoft Word + + + + \ No newline at end of file diff --git a/data/pds4/context_support/document/description/deepSpace1.docx b/data/pds4/context_support/document/description/deepSpace1.docx new file mode 100644 index 00000000..37f811b1 Binary files /dev/null and b/data/pds4/context_support/document/description/deepSpace1.docx differ diff --git a/data/pds4/context_support/document/description/deepSpace1.xml b/data/pds4/context_support/document/description/deepSpace1.xml new file mode 100644 index 00000000..135dae7d --- /dev/null +++ b/data/pds4/context_support/document/description/deepSpace1.xml @@ -0,0 +1,45 @@ + + + + + + urn:nasa:pds:context_support:document:ds1_description + 1.0 + Deep Space 1 Description + 1.22.0.0 + Product_Document + + 2024 + + This document provides an overview of the Deep Space 1 new technology + mission, including objectives, mission phases, encounters with (9660) + Braille and 19P/Borrelly, and extended missions. The content originated + on a NASA website about the mission and was included in the archive + with the permissio of the then-website curator and responsible party. + + + + + 2024-08-01 + 1.0 + + Creation by editing existing text. + + + + + + 2016 + + MSWord + English + 1 + + deepSpace1.docx + Microsoft Word + + + + \ No newline at end of file diff --git a/data/pds4/context_support/document/description/doubleAsteroidRedirectionTest.docx b/data/pds4/context_support/document/description/doubleAsteroidRedirectionTest.docx new file mode 100644 index 00000000..73a5b087 Binary files /dev/null and b/data/pds4/context_support/document/description/doubleAsteroidRedirectionTest.docx differ diff --git a/data/pds4/context_support/document/description/doubleAsteroidRedirectionTest.xml b/data/pds4/context_support/document/description/doubleAsteroidRedirectionTest.xml new file mode 100644 index 00000000..ce545a7f --- /dev/null +++ b/data/pds4/context_support/document/description/doubleAsteroidRedirectionTest.xml @@ -0,0 +1,49 @@ + + + + + + urn:nasa:pds:context_support:document:dart_description + 1.0 + Double Asteroid Redirection Test Description + 1.22.0.0 + Product_Document + + 2024 + + This document provides a brief description of the DART mission. + + + + Anne + Raugh + https://orcid.org/0000-0002-8300-9443 + + + + + + 2024-08-03 + 1.0 + + Creation from information in the version 1.0 investigation context product + by the same author. + + + + + + 2023 + + MCWord + English + 1 + + doubelAsteroidRedirectionTest.docx + Microsoft Word + + + + \ No newline at end of file diff --git a/data/pds4/context_support/document/description/epoxiEpochDixi.docx b/data/pds4/context_support/document/description/epoxiEpochDixi.docx new file mode 100644 index 00000000..08fdbfec Binary files /dev/null and b/data/pds4/context_support/document/description/epoxiEpochDixi.docx differ diff --git a/data/pds4/context_support/document/description/epoxiEpochDixi.xml b/data/pds4/context_support/document/description/epoxiEpochDixi.xml new file mode 100644 index 00000000..53e65c17 --- /dev/null +++ b/data/pds4/context_support/document/description/epoxiEpochDixi.xml @@ -0,0 +1,61 @@ + + + + + + urn:nasa:pds:context_support:document:epoxi_description + 1.0 + EPOXI (Combined DIXI and EPOCh) Description + 1.22.0.0 + Product_Document + + 2024 + + This document, extracted from the DESCRIPTION text of the PDS3 + mission catalog file and PDS4 version 1.0 mission context product, + provides an overview of the two Deep Impact spacecraft extended + missions, known collectively as "EPOXI". + + + + Anne + Raugh + https://orcid.org/0000-0002-8300-9443 + + + + + + 2024-08-04 + 1.0 + + Creation from existing sources: + + o The original text was converted to a formatted MS Word document. + o Typos were corrected. + o PDS3 REFERENCE_KEY_ID values were removed. + o Colliding citations were marked with 'a', 'b', etc., maintaining + PDS3-related sufffixes where they existed (PDS3 did not use the + 'a' suffix, but it has been added here). + o A bibliography was compiled based on citations in the text and + the references found in the PDS4 context object or PDS3 reference + database. + + + + + + 2024-08 + + MSWord + English + 1 + + epoxiEpochDixi.docx + Microsoft Word + + + + \ No newline at end of file diff --git a/data/pds4/context_support/document/description/giotto.docx b/data/pds4/context_support/document/description/giotto.docx new file mode 100644 index 00000000..fbe0f257 Binary files /dev/null and b/data/pds4/context_support/document/description/giotto.docx differ diff --git a/data/pds4/context_support/document/description/giotto.xml b/data/pds4/context_support/document/description/giotto.xml new file mode 100644 index 00000000..19679e7e --- /dev/null +++ b/data/pds4/context_support/document/description/giotto.xml @@ -0,0 +1,45 @@ + + + + + + urn:nasa:pds:context_support:document:giotto_description + 1.0 + Giotto Description + 1.22.0.0 + Product_Document + + 2024 + + This document was extracted from the DESCRIPTION text of the PDS3 + mission catalog file. + + + + + 2024-08-04 + 1.0 + + Creation. Typos that could be corrected have been. There is + one mangled sentence that could not be fixed, as several words + appear to be missing and it is not clear what those words might + have been. + + + + + + 1992 + + MSWord + English + 1 + + giotto.docx + Microsoft Word + + + + \ No newline at end of file diff --git a/data/pds4/context_support/document/description/hayabusa.docx b/data/pds4/context_support/document/description/hayabusa.docx new file mode 100644 index 00000000..164bbf0b Binary files /dev/null and b/data/pds4/context_support/document/description/hayabusa.docx differ diff --git a/data/pds4/context_support/document/description/hayabusa.xml b/data/pds4/context_support/document/description/hayabusa.xml new file mode 100644 index 00000000..db6fe9e9 --- /dev/null +++ b/data/pds4/context_support/document/description/hayabusa.xml @@ -0,0 +1,66 @@ + + + + + + urn:nasa:pds:context_support:document:hayabusa_description + 1.0 + Hayabusa Description + 1.22.0.0 + Product_Document + + + 2024 + + This document provides an overview of the Hayabusa mission and its + instruments. + + + + Donald + Yeomans + + + [unknown] + Semenov + + + + + Anne + Raugh + https://orcid.org/0000-0002-8300-9443 + + University of Maryland + + + + + + + + 2024-08-09 + 1.0 + + Created from the existing PDS3 mission catalog description "document". + Updated verb tenses and formatted for modern display and easier reading. + + + + + + + 2024-08-09 + + Updated and Formatted + English + 1 + + hayabusa.docx + Microsoft Word + + + + \ No newline at end of file diff --git a/data/pds4/context_support/document/description/ice.docx b/data/pds4/context_support/document/description/ice.docx new file mode 100644 index 00000000..5ee7d5f5 Binary files /dev/null and b/data/pds4/context_support/document/description/ice.docx differ diff --git a/data/pds4/context_support/document/description/ice.xml b/data/pds4/context_support/document/description/ice.xml new file mode 100644 index 00000000..96ad4b0f --- /dev/null +++ b/data/pds4/context_support/document/description/ice.xml @@ -0,0 +1,47 @@ + + + + + + + urn:nasa:pds:context_support:document:ice_description + 1.0 + International Sun-Earth Explorer-3/International Cometary Explorer Description + 1.22.0.0 + Product_Document + + + 2024 + + The bulk of this document is reformatted from the DESCRIPTION of the + PDS3 mission catalog file (c.1992), which was unattributed. A note was + added to the original text, summarizing the end of mission and 2014 + attempt to reclaim the spacecraft. + + + + Unknown Author + + + Anne + Raugh + https://orcid.org/0000-0002-8300-9443 + + + + + + 2024 + + MSWord + English + 1 + + ice.docx + Microsoft Word + + + + \ No newline at end of file diff --git a/data/pds4/context_support/document/description/iras.docx b/data/pds4/context_support/document/description/iras.docx new file mode 100644 index 00000000..4ac14b38 Binary files /dev/null and b/data/pds4/context_support/document/description/iras.docx differ diff --git a/data/pds4/context_support/document/description/iras.xml b/data/pds4/context_support/document/description/iras.xml new file mode 100644 index 00000000..12a3764c --- /dev/null +++ b/data/pds4/context_support/document/description/iras.xml @@ -0,0 +1,42 @@ + + + + + + urn:nasa:pds:context_support:document:iras_description + 1.0 + Infrared Astronomical Satellite Description + 1.22.0.0 + Product_Document + + 2024 + + This (uncredited) document was extracted from the DESCRIPTION text + of the PDS3 catalog file (c. 1992-4) and reformatted for modern document + handling. A small number of minor typos were corrected, and DOIs were + added for references that had acquired them. + + + + Anne + Raugh + https://orcid.org/0000-0002-8300-9443 + + + + + + + + MSWord + English + 1 + + iras.docx + Microsoft Word + + + + \ No newline at end of file diff --git a/data/pds4/context_support/document/description/iue.docx b/data/pds4/context_support/document/description/iue.docx new file mode 100644 index 00000000..75f23908 Binary files /dev/null and b/data/pds4/context_support/document/description/iue.docx differ diff --git a/data/pds4/context_support/document/description/iue.xml b/data/pds4/context_support/document/description/iue.xml new file mode 100644 index 00000000..2213094c --- /dev/null +++ b/data/pds4/context_support/document/description/iue.xml @@ -0,0 +1,43 @@ + + + + + + urn:nasa:pds:context_support:document:iue_description + 1.0 + International Ultraviolet Explorer Description + 1.22.0.0 + Product_Document + + 2024 + + This document provides a brief description of the IUE mission + and coverage, as originally presented in the PDS3 IUE mission + catalog file description area. + + + + + 2024-08-19 + 1.0 + + Created from existing text with minor updates to verb tenses. + + + + + + 1996 + + MSWord + English + 1 + + iue.docx + Microsoft Word + + + + \ No newline at end of file diff --git a/data/pds4/context_support/document/description/lowellObservatoryNearEarthObjectSurvey.docx b/data/pds4/context_support/document/description/lowellObservatoryNearEarthObjectSurvey.docx new file mode 100644 index 00000000..e12138af Binary files /dev/null and b/data/pds4/context_support/document/description/lowellObservatoryNearEarthObjectSurvey.docx differ diff --git a/data/pds4/context_support/document/description/lowellObservatoryNearEarthObjectSurvey.xml b/data/pds4/context_support/document/description/lowellObservatoryNearEarthObjectSurvey.xml new file mode 100644 index 00000000..58541c67 --- /dev/null +++ b/data/pds4/context_support/document/description/lowellObservatoryNearEarthObjectSurvey.xml @@ -0,0 +1,42 @@ + + + + + + urn:nasa:pds:context_support:document:loneos_description + 1.0 + Lowell Observatory Near Earth Object Survey Description + 1.22.0.0 + Product_Document + + 2024 + + This document contains a brief description of the LONEOS program, + extracted from the original context product for that investigation. + + + + + 2024-08-01 + 1.0 + + Creation + + + + + + 2024-08 + + MS Word + English + 1 + + lowellObservatoryNearEartObjectSurvey.docx + Microsoft Word + + + + \ No newline at end of file diff --git a/data/pds4/context_support/document/description/mm71.docx b/data/pds4/context_support/document/description/mm71.docx new file mode 100644 index 00000000..c777c85c Binary files /dev/null and b/data/pds4/context_support/document/description/mm71.docx differ diff --git a/data/pds4/context_support/document/description/mm71.xml b/data/pds4/context_support/document/description/mm71.xml new file mode 100644 index 00000000..cf07064e --- /dev/null +++ b/data/pds4/context_support/document/description/mm71.xml @@ -0,0 +1,43 @@ + + + + + + urn:nasa:pds:context_support:document:mm71_description + 1.0 + Mariner Mars '71 Description + 1.22.0.0 + Product_Document + + 2024 + + This document provides a brief description of the Mariner Mars '71 + project, comprising Mariners 8 and 9. Mission phase information is + included. + + + + + 2024-08-19 + 1.0 + + Created from existing text with minor updates for typos. + + + + + + 1996 + + MSWord + English + 1 + + mm71.docx + Microsoft Word + + + + \ No newline at end of file diff --git a/data/pds4/context_support/document/description/nearEarthAsteroidTracking.docx b/data/pds4/context_support/document/description/nearEarthAsteroidTracking.docx new file mode 100644 index 00000000..a55ffec8 Binary files /dev/null and b/data/pds4/context_support/document/description/nearEarthAsteroidTracking.docx differ diff --git a/data/pds4/context_support/document/description/nearEarthAsteroidTracking.xml b/data/pds4/context_support/document/description/nearEarthAsteroidTracking.xml new file mode 100644 index 00000000..4134bf16 --- /dev/null +++ b/data/pds4/context_support/document/description/nearEarthAsteroidTracking.xml @@ -0,0 +1,42 @@ + + + + + + urn:nasa:pds:context_support:document:neat_description + 1.0 + Near-Earth Asteroid Tracking Description + 1.22.0.0 + Product_Document + + 2024 + + This document contains the description of the NEAT survey extracted + from version 1.0 of the corresponding investigation context object. + + + + + 2024-07-31 + 1.0 + + Creation by reformatting unattributed text. + + + + + + 2024-08 + + MS Word + English + 1 + + nearEarthAsteroidTracking.docx + Microsoft Word + + + + \ No newline at end of file diff --git a/data/pds4/context_support/document/description/noSpecificInvestigation.docx b/data/pds4/context_support/document/description/noSpecificInvestigation.docx new file mode 100644 index 00000000..90632b73 Binary files /dev/null and b/data/pds4/context_support/document/description/noSpecificInvestigation.docx differ diff --git a/data/pds4/context_support/document/description/noSpecificInvestigation.xml b/data/pds4/context_support/document/description/noSpecificInvestigation.xml new file mode 100644 index 00000000..303236e3 --- /dev/null +++ b/data/pds4/context_support/document/description/noSpecificInvestigation.xml @@ -0,0 +1,53 @@ + + + + + + + urn:nasa:pds:context_support:document:none_description + 1.0 + No Specific Investigation Description + 1.22.0.0 + Product_Document + + + 2024 + + This document contains a brief description of the import and usual + use cases for the "No Specific Investigation" context product. + + + + Anne + Raugh + https://orcid.org/0000-0002-8300-9443 + + + + + + + 2024-07-31 + 1.0 + + Creation + + + + + + + 2024-08 + + MSWord + English + 1 + + noSpecificInvestigation.docx + Microsoft Word + + + + \ No newline at end of file diff --git a/data/pds4/context_support/document/description/spacewatch.docx b/data/pds4/context_support/document/description/spacewatch.docx new file mode 100644 index 00000000..fc3e64c5 Binary files /dev/null and b/data/pds4/context_support/document/description/spacewatch.docx differ diff --git a/data/pds4/context_support/document/description/spacewatch.xml b/data/pds4/context_support/document/description/spacewatch.xml new file mode 100644 index 00000000..6dbf9c34 --- /dev/null +++ b/data/pds4/context_support/document/description/spacewatch.xml @@ -0,0 +1,42 @@ + + + + + + urn:nasa:pds:context_support:document:spacewatch_description + 1.0 + Spacewatch Description + 1.22.0.0 + Product_Document + + 2024 + + This document contains the unattributed description of the Spacewatch group + extracted from version 1.0 of the associated context product. + + + + + 2024-07-31 + 1.0 + + Creation + + + + + + 2024-08 + + MSWord + English + 1 + + spacewatch.docx + Microsoft Word + + + + \ No newline at end of file diff --git a/data/pds4/context_support/document/description/~$epImpact.docx b/data/pds4/context_support/document/description/~$epImpact.docx new file mode 100644 index 00000000..883d8892 Binary files /dev/null and b/data/pds4/context_support/document/description/~$epImpact.docx differ diff --git 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+P,urn:nasa:pds:context_support:document:none_description::1.0 +P,urn:nasa:pds:context_support:document:spacewatch_description::1.0 + diff --git a/data/pds4/context_support/document/reference.txt b/data/pds4/context_support/document/reference.txt new file mode 100644 index 00000000..319b02b5 --- /dev/null +++ b/data/pds4/context_support/document/reference.txt @@ -0,0 +1,2276 @@ +PDS_VERSION_ID = PDS3 +LABEL_REVISION_NOTE = "2005-12-09, First Draft, A.Cardesin + 2007-01-26, 70 char line length, MB + 2007-08-31, Maud Barthelemy + 2007-09-05, Maud Barthelemy + 2008-02-08, Maud Barthelemy + 2008-04-22, Maud Barthelemy + 2008-05-09, MB, too long REF_KEY_ID + 2008-12-12, MB, 1 ref added + 2009-05-27, MB, NOTE added + 2009-06-17, MB, GULKIS + 2010-02-09, IR, GLASSMEIER toggled + 2010-04-21, MB, TROTT2009 + 2011-02-18, MB, editorial + 2011-06-06, MB, editorial and LAMYETAL2008 + 2012-01-31, MB, AST2 ref + 2012-03-12, MB, Typo line 46 and RPC MAG. + 2012-06-05, MB after AST2 review. + 2012-06-22, IR 3 bad chars removed. + 2012-12-17, MB PDS updates. + 2013-07-09, SBN:TB, added 4 shape model refs. + 2013-11-19, MB ERIKSSONETAL, EDBERGETAL2009 + 2015-01-23, MB after MISSION.CAT updates + 2015-02-03, MB slight updates + 2015-05-18, MB Miro ref added + 2015-07-03, MB RPC ICA ref added + 2015-07-14, MB GIADA ref added + 2015-08-26, MB RPCIES ref added + 2016-03-17, MB CHEOPS ref added + 2016-05-12, MB Giada 2016 added + 2016-05-20, MB Biele 2015 added + 2016-11-08, MB ALICE REF added + 2016-11-16, MB COSIMA added + 2016-11-30, MB RPCMAG added + 2017-01-24, MB SD2 added + 2017-06-01, EG RO-SGS-RP-1030, HANISCHETAL2001, + and STEPHAN2001 added. + 2017-08-18, MB CONSERT references + 2017-09-27, MB RMOC references. + 2018-02-22, MB CN references + 2018-03-02, MB remove JPL ref + 2018-04-26, MB COSAC + 2018-05-09, MB Typo Krueger + 2018-06-14, MB RPC MAG updates + 2018-08-10, MB SREM ref + 2018-08-21, M. Barthelemy SREM + 2018-08-29, M. Barthelemy SESAME. + 2019-07-17, DJH, DFA, VIRTIS and GIADA new references + and SREM typo fixes. + 2019-10-07, D. Fraga, Added SNODGRASSETAL2017 and + corrected typo in FILACCHIONEETAL2016 + 2020-12-09, DJH, Added reference for NAVCAM + calibration paper." + +RECORD_TYPE = "STREAM" + +NOTE = "This file is organised into two sections. The first half + contains the references common to all the instruments of + the ROSETTA mission. The second part contains the reference + specific to each instrument, in alphabetic order. The two + parts are separated by a comment + /*##### REFERENCES FROM THE INSTRUMENTS ########*/ . " + +OBJECT = REFERENCE + REFERENCE_KEY_ID = "ALTWEGGETAL2012" + REFERENCE_DESC = "Altwegg, K. et al., In situ mass spectrometry + during the Lutetia flyby, Planetary and Space Science 66, + 1, 173-178, 2012." +END_OBJECT = REFERENCE + +OBJECT = REFERENCE + REFERENCE_KEY_ID = "ANDREWSETAL2011" + REFERENCE_DESC = "Andrews, D. J. et al., Ptolemy Operations and + Results during the Rosetta flyby of Lutetia, EPSC-DPS Joint + Meeting 2011, Nantes, France, 2-7 October 2011." +END_OBJECT = REFERENCE + +OBJECT = REFERENCE + REFERENCE_KEY_ID = "BESSEL1999" + REFERENCE_DESC = "Bessell, M. S., Spectrophotometry: Revised + Standards and Techniques, Publ. Astron. Soc. Pac. 111, 1426, + 1999." +END_OBJECT = REFERENCE + +OBJECT = REFERENCE + REFERENCE_KEY_ID = "CREMONESEETAL2012" + REFERENCE_DESC = "Cremonese, G., et al., Hydrocode simulations of + the largest crater on asteroid Lutetia. Planetary and Space + Science 66, Issue 1, Pages 147-154, June 2012." +END_OBJECT = REFERENCE + +OBJECT = REFERENCE + REFERENCE_KEY_ID = "FORNASIERETAL2006" + REFERENCE_DESC = "Fornasier, S., I. Belskaya, M. Fulchignoni, + M.A. Barucci, and C. Barbieri, First albedo determination of 2867 + Steins, target of the Rosetta mission, Astron. Astrophys, 449, + L9-L12, 2006." +END_OBJECT = REFERENCE + +OBJECT = REFERENCE + REFERENCE_KEY_ID = "FUHRMANNETAL1998" + REFERENCE_DESC = "Fuhrmann, K., M.J. Pfeiffer, and J. Bernkopf, + F- and G-type stars with planetary companions: Andromedae, + 1 Cancri, Bootis, 16 Cygni and Coronae Borealis, + Astron. Astrophys., 336, 942-952, 1998." +END_OBJECT = REFERENCE + +OBJECT = REFERENCE + REFERENCE_KEY_ID = "GEIGERETAL2020" + REFERENCE_DESC = "Geiger B., R. Andres, and T. Statella, Radiometric + Calibration of the Rosetta Navigation Camera, Journal of + Astronomical Instrumentation, in revision, 2020." +END_OBJECT = REFERENCE + +OBJECT = REFERENCE + REFERENCE_KEY_ID = "GLASSMEIERETAL2007A" + REFERENCE_DESC = "Glassmeier, K.H., H. Boehnhardt, D. Koschny, + E. Kuhrt, and I. Richter, The Rosetta Mission: Flying Towards + the Origin of the Solar System, Space Science Reviews, 128(1-4), + 1-21, Feb. 2007." +END_OBJECT = REFERENCE + +OBJECT = REFERENCE + REFERENCE_KEY_ID = "HAMUYETAL1992" + REFERENCE_DESC = "Hamuy, M. et al., Southern spectrophotometric + standards. I, Publ. Astron. Soc. Pac. 104, 533, 1992." +END_OBJECT = REFERENCE + +OBJECT = REFERENCE + REFERENCE_KEY_ID = "HAMUYETAL1994" + REFERENCE_DESC = "Hamuy, M. et al., Southern spectrophotometric + standards. II, Publ. Astron. Soc. Pac. 106, 566, 1994." +END_OBJECT = REFERENCE + +OBJECT = REFERENCE + REFERENCE_KEY_ID = "HANSENETAL2007" + REFERENCE_DESC = "Hansen, K.C., T. Bagdonat, U. Motschmann, + C. Alexander, M.R. Combi, T.E. Cravens, T.I. Gombosi, + Y.-D. Jia, and I.P. Robertson, The Plasma Environment of Comet + 67P/Churyumov-Gerasimenko Throughout the Rosetta Main Mission, + Space Science Reviews, 128(1-4), 133-166, Feb. 2007." +END_OBJECT = REFERENCE + +OBJECT = REFERENCE + REFERENCE_KEY_ID = "KOSCHNYETAL2007" + REFERENCE_DESC = "Koschny, D, V. Dhiri, K. Wirth, J. Zender, + R. Solaz, R. Hoofs, R. Laureijs, T.-M Ho, B. Davidsson, and + G. Schwehm, Scientific Planning and Commanding of the Rosetta + Payload, Space Sci. Rev., 128(1-4), 167-188, Feb. 2007." +END_OBJECT = REFERENCE + +OBJECT = REFERENCE + REFERENCE_KEY_ID = "KUPPERSETAL2007" + REFERENCE_DESC = "Kuppers, M. et al., Determination of the light + curve of the Rosetta target asteroid (2867) Steins by the OSIRIS + cameras onboard Rosetta, Astron. Astrophys, Vol. 462-1, pL13-L16, + January 2007." +END_OBJECT = REFERENCE + +OBJECT = REFERENCE + REFERENCE_KEY_ID = "KUPPERSETAL2012" + REFERENCE_DESC = "Kuppers, M. et al., Boulders on Lutetia, + Planetary and Space Science, 66, 71-78, May 2012." +END_OBJECT = REFERENCE + +OBJECT = REFERENCE + REFERENCE_KEY_ID = "LANG1992" + REFERENCE_DESC = "Lang, K.R., Astrophysical Data: Planets and + Stars, Springer-Verlag, New York, Incorporated, 1992." +END_OBJECT = REFERENCE + +OBJECT = REFERENCE + REFERENCE_KEY_ID = "LANDOLT1992" + REFERENCE_DESC = "Landolt A.U., + UBVRI Photometric Standard Stars in the Magnitude Range + 11.5 + + + + + urn:nasa:pds:context_support:image:comet_borrelly_nucleus + 1.0 + Comet Borrelly Nucleus as Imaged by Deep Space 1 + 1.22.0.0 + Product_Document + + 2001 + + In this high resolution view of the icy, rocky nucleus of comet Borrelly, (about 45 meters + or 150 feet per pixel) a variety of terrains and surface textures, mountains and fault + structures, and darkened material are visible over the nucleus's surface. This was the + final image of the nucleus of comet Borrelly, taken just 160 seconds before Deep Space 1's + closest approach to it. This image shows the 8-km (5-mile) long nucleus about 3417 kilometers + (over 2,000 miles) away. + + + + NASA/JPL + + + + + + 2001-09-22 + + Image + English + 1 + + This file and its caption were downloaded from Wikimedia Commons. + + + Comet_Borrelly_Nucleus.jpg + JPEG + + + + \ No newline at end of file diff --git a/data/pds4/context_support/image/Dawn_assembly_at_KSC.jpg b/data/pds4/context_support/image/Dawn_assembly_at_KSC.jpg new file mode 100644 index 00000000..021f9812 Binary files /dev/null and b/data/pds4/context_support/image/Dawn_assembly_at_KSC.jpg differ diff --git a/data/pds4/context_support/image/Dawn_assembly_at_KSC.xml b/data/pds4/context_support/image/Dawn_assembly_at_KSC.xml new file mode 100644 index 00000000..d8e0ced0 --- /dev/null +++ b/data/pds4/context_support/image/Dawn_assembly_at_KSC.xml @@ -0,0 +1,53 @@ + + + + + + urn:nasa:pds:context_support:image:dawn_assembly_at_ksc + 1.0 + Dawn Spacecraft Assembly at Kennedy Space Center + 1.22.0.0 + Product_Document + + 2007 + + The Dawn spacecraft is seen here in clean room C of Astrotech's Payload + Processing Facility. In the clean room, the spacecraft will undergo further + processing. Dawn's mission is to explore two of the asteroid belt's most + intriguing and dissimilar occupants: asteroid Vesta and the dwarf planet Ceres. + + + + George + Shelton + + NASA + + + + + + + 2024-08-01 + 1.0 + + Image and description downloaded from Wikimedia Commons. + + + + + + 2007-04-11 + + Image + English + 1 + + Dawn_assembly_at_KSC.jpg + JPEG + + + + \ No newline at end of file diff --git a/data/pds4/context_support/image/Dawn_logo.png b/data/pds4/context_support/image/Dawn_logo.png new file mode 100644 index 00000000..e9a85eb5 Binary files /dev/null and b/data/pds4/context_support/image/Dawn_logo.png differ diff --git a/data/pds4/context_support/image/Dawn_logo.xml b/data/pds4/context_support/image/Dawn_logo.xml new file mode 100644 index 00000000..5dbb971e --- /dev/null +++ b/data/pds4/context_support/image/Dawn_logo.xml @@ -0,0 +1,41 @@ + + + + + + urn:nasa:pds:context_support:image:dawm_mission_logo + 1.0 + Dawn Mission Logo + 1.22.0.0 + Product_Document + + 2007 + + Mission logo for the Dawn spacecraft. Photojournal ID: PIA19375 + + + + + 2024-08-01 + 1.0 + + Downloaded and labeled + + + + + + 2007-09-01 + + Graphic + English + 1 + + Dawn_logo.png + PNG + + + + \ No newline at end of file diff --git a/data/pds4/context_support/image/collection.xml b/data/pds4/context_support/image/collection.xml new file mode 100644 index 00000000..77fdb60e --- /dev/null +++ b/data/pds4/context_support/image/collection.xml @@ -0,0 +1,62 @@ + + + + + + urn:nasa:pds:context_support:image + 1.0 + Context Product Support Images and Graphics + 1.22.0.0 + Product_Collection + + 2024 + + This collection contains images and graphics to be used in + supporting display and use of context products. + + + + + 2024-08-01 + 1.0 + + Creation + + + + + + Document + + + + inventory.csv + + + 0 + PDS DSV 1 + 5 + Carriage-Return Line-Feed + Comma + + 2 + 0 + + Member Status + 1 + ASCII_String + 1 + + + LIDVID_LID + 2 + ASCII_LIDVID_LID + 255 + + + inventory_has_member_product + + + \ No newline at end of file diff --git a/data/pds4/context_support/image/contour_KSC-02pd0951.jpg b/data/pds4/context_support/image/contour_KSC-02pd0951.jpg new file mode 100644 index 00000000..bbabeef3 Binary files /dev/null and b/data/pds4/context_support/image/contour_KSC-02pd0951.jpg differ diff --git a/data/pds4/context_support/image/contour_KSC-02pd0951.xml b/data/pds4/context_support/image/contour_KSC-02pd0951.xml new file mode 100644 index 00000000..a4c324ad --- /dev/null +++ b/data/pds4/context_support/image/contour_KSC-02pd0951.xml @@ -0,0 +1,58 @@ + + + + + + urn:nasa:pds:context_support:image:contour_ksc02pd0951 + 1.0 + CONTOUR Spacecraft on Display at the Spacecraft Assembly and Encapsulation Facility at Kennedy Space Center + 1.22.0.0 + Product_Document + + 2002 + + Caption from https://images.nasa.gov/details/KSC-02pd0951: + + KENNEDY SPACE CENTER, FLA. -- The Comet Nucleus Tour (CONTOUR) spacecraft is on + display for the media in the Spacecraft Assembly and Encapsulation Facility 2. + CONTOUR will provide the first detailed look into the heart of a comet -- the + nucleus. Flying as close as 60 miles (100 kilometers) to at least two comets, + the spacecraft will take the sharpest pictures yet of a nucleus while analyzing + the gas and dust that surround them. CONTOUR is scheduled for launch aboard a + Delta II rocket July 1, 2002, from Launch Complex 17-A, Cape Canaveral Air + Force Station. + + + + + 2024-08-01 + 1.0 + + Downloaded image and labeled. + + + + + Public Domain + + + urn:nasa:pds:bundle:context:null + product_to_license + + + + + 2002-06-05 + + Image + English + 1 + + comet_KSC-02pd0951.jpg + JPEG + + + + \ No newline at end of file diff --git a/data/pds4/context_support/image/inventory.csv b/data/pds4/context_support/image/inventory.csv new file mode 100644 index 00000000..a5e7bc12 --- /dev/null +++ b/data/pds4/context_support/image/inventory.csv @@ -0,0 +1,4 @@ +P,urn:nasa:pds:context_support:image:contour_ksc02pd0951::1.0 +P,urn:nasa:pds:context_support:image:comet_borrelly_nucleus::1.0 +P,urn:nasa:pds:context_support:image:dawn_assembly_at_ksc::1.0 +P,urn:nasa:pds:context_support:image:dawm_mission_logo::1.0 diff --git a/data/pds4/context_support/iras.docx b/data/pds4/context_support/iras.docx new file mode 100644 index 00000000..4ac14b38 Binary files /dev/null and b/data/pds4/context_support/iras.docx differ