PDS_VERSION_ID = PDS3 LABEL_REVISION_NOTE = "2016-12-05, SONC, version 1.0" /* PVV version 3.13 */ /* Edited Science data */ /* FILE CHARACTERISTIC DATA ELEMENTS */ RECORD_TYPE = FIXED_LENGTH FILE_RECORDS = 53970 RECORD_BYTES = 65 FILE_NAME = "MAG_FS2_140410111506_00017.TAB" /* DATA OBJECT POINTERS */ ^ROMAP_MAG_RAWSC_TABLE = ("MAG_FS2_140410111506_00017.TAB",1 ) DATA_SET_ID = "RL-CAL-ROMAP-2-PHC-MAG-V1.0" DATA_SET_NAME = "ROSETTA-LANDER CAL ROMAP 2 PHC MAG V1.0" PRODUCT_ID = "MAG_FS2_140410111506_00017" PRODUCT_CREATION_TIME = 2016-12-05T13:11:08 MISSION_NAME = "INTERNATIONAL ROSETTA MISSION" MISSION_PHASE_NAME = "POST HIBERNATION COMMISSIONING" MISSION_ID = ROSETTA INSTRUMENT_HOST_NAME = "ROSETTA-LANDER" INSTRUMENT_HOST_ID = RL OBSERVATION_TYPE = "POST HIBERNATION COMMISSIONING" PRODUCT_TYPE = EDR START_TIME = 2014-04-10T11:15:06.509 STOP_TIME = 2014-04-10T11:32:32.790 SPACECRAFT_CLOCK_START_COUNT = "3/355749241.24" SPACECRAFT_CLOCK_STOP_COUNT = "3/355750288.01" 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 = "CALIBRATION" TARGET_TYPE = "CALIBRATION" PROCESSING_LEVEL_ID = "2" DATA_QUALITY_ID = "4" DATA_QUALITY_DESC = "4: absolute error exceed 100 nT" /* GEOMETRY PARAMETERS */ /* SPACECRAFT LOCATION: Position */ SC_SUN_POSITION_VECTOR = ( -102488060.7, 540363934.9, 298633537.4) /* TARGET PARAMETERS: Position , Velocity */ SC_TARGET_POSITION_VECTOR = ( -1353919.1, -3339070.9, -848295.6) SC_TARGET_VELOCITY_VECTOR = ( 288.179,702.360,173.256) /* SPACECRAFT POSITION WITH RESPECT TO CENTRAL BODY */ SPACECRAFT_ALTITUDE = 3701632.4 SUB_SPACECRAFT_LATITUDE = -16.66 SUB_SPACECRAFT_LONGITUDE = 142.40 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_RAWSC_TABLE NAME = "ROMAP_MAG EDITED SCIENCE DATA" INTERCHANGE_FORMAT = ASCII ROWS = 53970 COLUMNS = 5 ROW_BYTES = 65 ^STRUCTURE = "ROMAP_MAG_RAWSC.FMT" END_OBJECT = ROMAP_MAG_RAWSC_TABLE END