PDS_VERSION_ID = PDS3 LABEL_REVISION_NOTE = "2015-07-08, SONC, version 1.0" /* PVV version 3.8 */ /* Calibrated SC data before PEN deployment (Level 3 LAB) */ /* FILE CHARACTERISTIC DATA ELEMENTS */ RECORD_TYPE = FIXED_LENGTH RECORD_BYTES = 152 FILE_RECORDS = 4586 FILE_NAME = "MUP_MAPS3B_141112073642.TAB" /* DATA OBJECT POINTERS */ ^MAP_3B_TABLE = ("MUP_MAPS3B_141112073642.TAB",1 ) DATA_SET_ID = "RL-C-MUPUS-3-SDL-V1.0" DATA_SET_NAME = "ROSETTA-LANDER 67P MUPUS 3 SDL V1.0" PRODUCT_ID = "MUP_MAPS3B_141112073642" PRODUCT_CREATION_TIME = 2015-07-08T14:52:55 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 = RDR START_TIME = 2014-11-12T07:36:42.884 STOP_TIME = 2014-11-12T14:48:34.965 SPACECRAFT_CLOCK_START_COUNT = "3/374398531.48" SPACECRAFT_CLOCK_STOP_COUNT = "3/374424443.52" PRODUCER_ID = "SONC" PRODUCER_FULL_NAME = "SCIENCE OPERATIONS AND NAVIGATION CENTER" PRODUCER_INSTITUTION_NAME = "CNES" INSTRUMENT_ID = MUPUS INSTRUMENT_NAME ="MULTI PURPOSE SUITE FOR SURFACE AND SUBSURFACE SCIENCE" INSTRUMENT_TYPE = {"PENETROMETER THERMAL PROBE","INFRARED RADIOMETER","ACCELEROMETER"} INSTRUMENT_MODE_ID = "N/A" INSTRUMENT_MODE_DESC = "N/A" TARGET_NAME = "67P/CHURYUMOV-GERASIMENKO 1 (1969 R1)" TARGET_TYPE = "COMET" PROCESSING_LEVEL_ID = "3" DATA_QUALITY_ID = "42441" DATA_QUALITY_DESC = "SEPARATE QUALITY FOR 4 TM channels and ANC-T 'ABCDT'" /* GEOMETRY PARAMETERS */ /* SPACECRAFT LOCATION: Position */ SC_SUN_POSITION_VECTOR = ( -242369489.7, 321055165.7, 196388841.3) /* TARGET PARAMETERS: Position , Velocity */ SC_TARGET_POSITION_VECTOR = ( -12.7, -22.1, -1.1) SC_TARGET_VELOCITY_VECTOR = ( 0.574, 0.616, 0.054) /* SPACECRAFT POSITION WITH RESPECT TO CENTRAL BODY */ SPACECRAFT_ALTITUDE = 23.6 SUB_SPACECRAFT_LATITUDE = -12.49 SUB_SPACECRAFT_LONGITUDE = 48.01 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 " /* SD2 PARAMETERS */ ROSETTA:SD2_OVEN_FILLING = "N/A" ROSETTA:SD2_DRILL_DEPTH = 999.99 ROSETTA:SD2_OVEN_NUMBER = 99 ROSETTA:SD2_OVEN_TYPE = "N/A" ROSETTA:SAMPLE_NUMBER = 99 ROSETTA:SAMPLE_TAPPING = "N/A" ROSETTA:SAMPLE_VOLUME = 999.99 /* DATA OBJECT DEFINITION */ OBJECT = MAP_3B_TABLE NAME = "MAP_3B" INTERCHANGE_FORMAT = ASCII ROWS = 4586 COLUMNS = 16 ROW_BYTES = 152 ^STRUCTURE = "MAP_3B.FMT" END_OBJECT = MAP_3B_TABLE END END