A dataset provided by the European Space Agency

URL ftp://psa.esac.esa.int/pub/mirror/pub/mirror/INTERNATIONAL-ROSETTA-MISSION/VIRTIS/RO-C-VIRTIS-2-EXT3-MTP032-V2.0
DOI https://doi.org/10.5270/esa-j15l5mt
Abstract This release contains the digital numbers (DN) contained in the telemetry (TM) packages of the VIRTIS instrument on board of the spacecraft Rosetta. This volume contains data at the vicinity of comet 67P, from the EXTENSION 3 MTP032 phase, which occurred from 2016-07-27 to 2016-08-10. This version of the dataset (2.0) is produced by a fixed EGSE software. The old version of the software produced incomplete products, reduced by one line
Description Required Reading The format of all VIRTIS data are described in detail by the EAICD document located in the /DOCUMENT directory. VIRTIS team strongly recommends reading this documentation before using the data. Data Set Overview = This data set contains raw data acquired by the Rosetta Orbiter VIRTIS spectrometer during the EXTENSION 3 MTP032 of the Rosetta mission. Processing The data in this data set are raw, CODMAC Level 2 data. As such, the data has been calibrated. Data The data are in PDS format. A detailed description of the data format is given in the VIRTIS EAICD document located in the DOCUMENT directory of this data set. Ancillary Data No ancillary data included in this data set. Coordinate System = The geometry items SC_SUN_POSITION_VECTOR, SC_TARGET_POSITION_VECTOR and SC_TARGET_VELOCITY_VECTOR provided in the label of the data product are relative to the Earth Mean Equator frame of J2000. <>_SPACECRAFT_LATITUDE, <>_SPACECRAFT_LONGITUDE are given in the PLANETOCENTRIC coordinate system. These parameters are corrected by planetary and stellar aberrations. Distances are given in km, angles in degrees. Software The data can be accessed with the software IDL routines provided and documented in the EXTRAS directory. History = Version 1.0 - First data delivery Version 2.0 - Fixed a bug in the EGSE software. The old version of the software produced incomplete products, reduced by one line.
Instrument VIRTIS
Temporal Coverage 2016-07-27T02:25:00Z/2016-08-10T02:24:59Z
Version V2.0
Mission Description 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 ...
Creator Contact CAPACCIONI
Date Published 2020-12-14
Publisher And Registrant European Space Agency
Credit Guidelines European Space Agency, 2020-12-14, RO-C-VIRTIS-2-EXT3-MTP032, V2.0. https://doi.org/10.5270/esa-j15l5mt