PDS_VERSION_ID = PDS3 LABEL_REVISION_NOTE = "2016-12-14, SONC, version 1.0" /* PVV version 3.13 */ /* Edited Science data */ /* FILE CHARACTERISTIC DATA ELEMENTS */ RECORD_TYPE = FIXED_LENGTH FILE_RECORDS = 43140 RECORD_BYTES = 65 FILE_NAME = "MAG_FS2_141112033507_00718.TAB" /* DATA OBJECT POINTERS */ ^ROMAP_MAG_RAWSC_TABLE = ("MAG_FS2_141112033507_00718.TAB",1 ) DATA_SET_ID = "RL-C-ROMAP-2-SDL-MAG-V1.0" DATA_SET_NAME = "ROSETTA-LANDER 67P ROMAP 2 SDL MAG V1.0" PRODUCT_ID = "MAG_FS2_141112033507_00718" PRODUCT_CREATION_TIME = 2016-12-14T16:44:25 MISSION_NAME = "INTERNATIONAL ROSETTA MISSION" MISSION_PHASE_NAME = "SEPARATION DESCENT LANDING" MISSION_ID = ROSETTA INSTRUMENT_HOST_NAME = "ROSETTA-LANDER" INSTRUMENT_HOST_ID = RL OBSERVATION_TYPE = "SEPARATION DESCENT LANDING" PRODUCT_TYPE = EDR START_TIME = 2014-11-12T03:35:07.176 STOP_TIME = 2014-11-12T15:34:05.721 SPACECRAFT_CLOCK_START_COUNT = "3/374384036.01" SPACECRAFT_CLOCK_STOP_COUNT = "3/374427174.18" 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 = "2" DATA_QUALITY_ID = "4" DATA_QUALITY_DESC = "4: Absolute error exceed 100 nT" /* GEOMETRY PARAMETERS */ /* SPACECRAFT LOCATION: Position */ SC_SUN_POSITION_VECTOR = ( -242288342.0, 321282368.9, 196500784.3) /* TARGET PARAMETERS: Position , Velocity */ SC_TARGET_POSITION_VECTOR = ( -16.2, -24.9, -2.7) SC_TARGET_VELOCITY_VECTOR = ( 0.046,-0.044, 0.134) /* SPACECRAFT POSITION WITH RESPECT TO CENTRAL BODY */ SPACECRAFT_ALTITUDE = 27.9 SUB_SPACECRAFT_LATITUDE = -13.53 SUB_SPACECRAFT_LONGITUDE = 319.33 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 = 43140 COLUMNS = 5 ROW_BYTES = 65 ^STRUCTURE = "ROMAP_MAG_RAWSC.FMT" END_OBJECT = ROMAP_MAG_RAWSC_TABLE END