PDS_VERSION_ID = PDS3 LABEL_REVISION_NOTE = "2017-01-11, SONC, version 1.0 2018-04-24, LPC2E, N. TRAORE, version 2.0" /* PVV version 3.13 */ /* Calibrated HK data (Level 3) */ /* FILE CHARACTERISTIC DATA ELEMENTS */ RECORD_TYPE = FIXED_LENGTH RECORD_BYTES = 69 FILE_RECORDS = 24956 FILE_NAME = "RPCMIPH3XXX0809010009_13309.TAB" /* DATA OBJECT POINTERS */ ^CALIBRATED_HK_TABLE = ("RPCMIPH3XXX0809010009_13309.TAB",1 ) DATA_SET_ID = "RO-A-RPCMIP-3-AST1-V2.0" DATA_SET_NAME = "ROSETTA-ORBITER STEINS RPCMIP 3 AST1 V2.0" DATA_SET_PARAMETER_NAME = "HOUSEKEEPING PARAMETERS" CALIBRATION_SOURCE_ID = "RPCMIP" PRODUCT_ID = "RPCMIPH3XXX0809010009_13309" PRODUCT_CREATION_TIME = 2018-05-04T09:48:07.000 MISSION_ID = ROSETTA MISSION_NAME = "INTERNATIONAL ROSETTA MISSION" MISSION_PHASE_NAME = "STEINS FLY-BY" INSTRUMENT_HOST_ID = RO INSTRUMENT_HOST_NAME = "ROSETTA-ORBITER" OBSERVATION_TYPE = "STEINS FLYBY" PRODUCT_TYPE = RDR START_TIME = 2008-09-01T00:09:43.496 STOP_TIME = 2008-09-10T05:59:35.644 SPACECRAFT_CLOCK_START_COUNT = "1/178848546.01653" SPACECRAFT_CLOCK_STOP_COUNT = "1/179647138.01653" PRODUCER_ID = {"LPC2E", "SONC"} PRODUCER_FULL_NAME = {"LAB DE PHYSIQUE ET CHIMIE DE L'ENVIRONNEMENT ET DE L'ESPACE", "SCIENCE OPERATIONS AND NAVIGATION CENTER"} PRODUCER_INSTITUTION_NAME = {"CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE", "CNES"} INSTRUMENT_ID = RPCMIP INSTRUMENT_NAME = "ROSETTA PLASMA CONSORTIUM - MUTUAL IMPEDANCE PROBE" INSTRUMENT_TYPE = "PLASMA ANALYZER" INSTRUMENT_MODE_ID = "N/A" INSTRUMENT_MODE_DESC = "N/A" ^RPC_SCIENCE_USAGE_DESC = "RPC_USER_GUIDE.PDF" ^RPCMIP_SCIENCE_USAGE_DESC = "RPC-MIP-UG-LPC2E.PDF" TARGET_NAME = "2867 STEINS" TARGET_TYPE = "ASTEROID" PROCESSING_LEVEL_ID = 3 DATA_QUALITY_ID = "0" DATA_QUALITY_DESC = "0 : Good quality" /* GEOMETRY PARAMETERS */ /* SPACECRAFT LOCATION: Position */ SC_SUN_POSITION_VECTOR = ( 112582879.9, 266876918.6, 130357579.2) /* TARGET PARAMETERS: Position , Velocity */ SC_TARGET_POSITION_VECTOR = ( -2937344.9, -1972614.5, -305151.4) SC_TARGET_VELOCITY_VECTOR = ( 7128.091,4787.912,741.089) /* SPACECRAFT POSITION WITH RESPECT TO CENTRAL BODY */ SPACECRAFT_ALTITUDE = 3551380.2 SUB_SPACECRAFT_LATITUDE = -5.18 SUB_SPACECRAFT_LONGITUDE = 27.83 NOTE = "The values of the keywords SC_SUN_POSITION_VECTOR, SC_TARGET_POSITION_VECTOR and SC_TARGET_VELOCITY_VECTOR are related to the equatorial J2000 inertial frame (EMEJ200). The values of SUB_SPACECRAFT_LATITUDE and SUB_SPACECRAFT_LONGITUDE are northern latitude and eastern longitude in the standard planetocentric IAU_ frame. All values are computed for the time = START_TIME. Distances are given in velocities in , angles in " /* DATA OBJECT DEFINITION */ OBJECT = CALIBRATED_HK_TABLE NAME = "CALIBRATED_HK" INTERCHANGE_FORMAT = ASCII ROWS = 24956 COLUMNS = 7 ROW_BYTES = 69 ^STRUCTURE = "MIP_CALIBRATED_HK.FMT" END_OBJECT = CALIBRATED_HK_TABLE END