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 */ /* Configuration Tables */ /* FILE CHARACTERISTIC DATA ELEMENTS */ RECORD_TYPE = FIXED_LENGTH RECORD_BYTES = 283 FILE_RECORDS = 2 FILE_NAME = "RPCMIPS3XXX0901312232_00009.TAB" /* DATA OBJECT POINTERS */ ^CONFIG_TABLE_TABLE = ("RPCMIPS3XXX0901312232_00009.TAB",1 ) DATA_SET_ID = "RO-CAL-RPCMIP-3-CR4B-V1.0" DATA_SET_NAME = "ROSETTA-ORBITER CAL RPCMIP 3 CR4B V1.0" DATA_SET_PARAMETER_NAME = "OPERATIONAL PARAMETERS" CALIBRATION_SOURCE_ID = "RPCMIP" PRODUCT_ID = "RPCMIPS3XXX0901312232_00009" PRODUCT_CREATION_TIME = 2018-05-07T15:10:48.000 MISSION_ID = ROSETTA MISSION_NAME = "INTERNATIONAL ROSETTA MISSION" MISSION_PHASE_NAME = "CRUISE 4-2" INSTRUMENT_HOST_ID = RO INSTRUMENT_HOST_NAME = "ROSETTA-ORBITER" OBSERVATION_TYPE = "CRUISE 4-2" PRODUCT_TYPE = RDR START_TIME = 2009-01-31T22:32:16.833 STOP_TIME = 2009-01-31T22:41:52.833 SPACECRAFT_CLOCK_START_COUNT = "1/192061898.01653" SPACECRAFT_CLOCK_STOP_COUNT = "1/192062474.01653" 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 = "CALIBRATION" TARGET_TYPE = "CALIBRATION" PROCESSING_LEVEL_ID = 3 DATA_QUALITY_ID = "0" DATA_QUALITY_DESC = "0 : Good quality" /* GEOMETRY PARAMETERS */ /* SPACECRAFT LOCATION: Position */ SC_SUN_POSITION_VECTOR = ( -79131962.8, 282257416.7, 161451923.8) /* TARGET PARAMETERS: Position , Velocity */ SC_TARGET_POSITION_VECTOR = ("N/A", "N/A", "N/A") SC_TARGET_VELOCITY_VECTOR = ("N/A", "N/A", "N/A") /* SPACECRAFT POSITION WITH RESPECT TO CENTRAL BODY */ SPACECRAFT_ALTITUDE = "N/A" SUB_SPACECRAFT_LATITUDE = "N/A" SUB_SPACECRAFT_LONGITUDE = "N/A" 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 = CONFIG_TABLE_TABLE NAME = "CONFIG_TABLE" INTERCHANGE_FORMAT = ASCII ROWS = 2 COLUMNS = 21 ROW_BYTES = 283 ^STRUCTURE = "MIP_CONFIG_TABLE.FMT" END_OBJECT = CONFIG_TABLE_TABLE END