PDS_VERSION_ID = PDS3 LABEL_REVISION_NOTE = "2016-12-14, SONC, version 1.0" /* PVV version 3.13 */ /* Calibrated in Instrument coordinates (Level 5) */ /* FILE CHARACTERISTIC DATA ELEMENTS */ RECORD_TYPE = FIXED_LENGTH FILE_RECORDS = 7170 RECORD_BYTES = 119 FILE_NAME = "MAG_FSE_141113083307_00119.TAB" /* DATA OBJECT POINTERS */ ^ROMAP_MAG_CALSCE_TABLE = ("MAG_FSE_141113083307_00119.TAB",1 ) DATA_SET_ID = "RL-C-ROMAP-5-FSS-MAG-V1.0" DATA_SET_NAME = "ROSETTA-LANDER 67P ROMAP 5 FSS MAG V1.0" PRODUCT_ID = "MAG_FSE_141113083307_00119" PRODUCT_CREATION_TIME = 2016-12-14T12:55:56 MISSION_NAME = "INTERNATIONAL ROSETTA MISSION" MISSION_PHASE_NAME = "FIRST SCIENCE SEQUENCE" MISSION_ID = ROSETTA INSTRUMENT_HOST_NAME = "ROSETTA-LANDER" INSTRUMENT_HOST_ID = RL OBSERVATION_TYPE = "FIRST SCIENCE SEQUENCE" PRODUCT_TYPE = RDR START_TIME = 2014-11-13T08:33:07.000 STOP_TIME = 2014-11-13T10:32:36.000 SPACECRAFT_CLOCK_START_COUNT = "3/374488315.29" SPACECRAFT_CLOCK_STOP_COUNT = "3/374495484.53" PRODUCER_ID = "SONC" PRODUCER_FULL_NAME = "SCIENCE OPERATIONS AND NAVIGATION CENTER" PRODUCER_INSTITUTION_NAME = "CNES" INSTRUMENT_ID = ROMAP INSTRUMENT_NAME = "ROSETTA LANDER MAGNETOMETER AND PLASMA MONITOR" INSTRUMENT_TYPE = {"FLUXGATE MAGNETOMETER","ELECTROSTATIC ANALYZER", "FARADAY CUP"} DETECTOR_ID = MAG INSTRUMENT_MODE_ID = "N/A" INSTRUMENT_MODE_DESC = "N/A" TARGET_NAME = "67P/CHURYUMOV-GERASIMENKO 1 (1969 R1)" TARGET_TYPE = "COMET" PROCESSING_LEVEL_ID = "5" DATA_QUALITY_ID = "1" DATA_QUALITY_DESC = "1 : Absolute error less than 1 nT" /* GEOMETRY PARAMETERS */ /* SPACECRAFT LOCATION: Position */ SC_SUN_POSITION_VECTOR = ( -242870383.3, 319645769.9, 195694138.1) /* TARGET PARAMETERS: Position , Velocity */ SC_TARGET_POSITION_VECTOR = ( 15.3, 3.1, -13.4) SC_TARGET_VELOCITY_VECTOR = ( 0.082, 0.420,-0.246) /* SPACECRAFT POSITION WITH RESPECT TO CENTRAL BODY */ SPACECRAFT_ALTITUDE = 18.7 SUB_SPACECRAFT_LATITUDE = -15.15 SUB_SPACECRAFT_LONGITUDE = 284.73 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 = ROMAP_MAG_CALSCE_TABLE NAME = "ROMAP_MAG_CALSCE" INTERCHANGE_FORMAT = ASCII ROWS = 7170 COLUMNS = 8 ROW_BYTES = 119 ^STRUCTURE = "ROMAP_MAG_CALSCE.FMT" END_OBJECT = ROMAP_MAG_CALSCE_TABLE END