PDS_VERSION_ID = PDS3 LABEL_REVISION_NOTE = "2017-03-06, SONC, version 1.0" /* PVV version 3.13 */ /* Edited SC data from DIM Noise Test Mode (SONC Level 2) */ RECORD_TYPE = FIXED_LENGTH FILE_RECORDS = 3 RECORD_BYTES = 49 FILE_NAME = "SES_FS2_DNT_1404141726.TAB" /* DATA OBJECT POINTERS */ ^NT_TABLE = ("SES_FS2_DNT_1404141726.TAB",1 ) DATA_SET_ID = "RL-CAL-SESAME-2-PHC-V1.0" DATA_SET_NAME = "ROSETTA-LANDER CAL SESAME 2 PHC V1.0" PRODUCT_ID = "SES_FS2_DNT_1404141726" PRODUCT_CREATION_TIME = 2017-03-06T15:48:41 MISSION_NAME = "INTERNATIONAL ROSETTA MISSION" MISSION_PHASE_NAME = "POST HIBERNATION COMMISSIONING" MISSION_ID = ROSETTA INSTRUMENT_HOST_NAME = "ROSETTA-LANDER" INSTRUMENT_HOST_ID = RL PRODUCT_TYPE = EDR START_TIME = 2014-04-14T17:26:34.551 STOP_TIME = 2014-04-14T17:30:13.551 SPACECRAFT_CLOCK_START_COUNT = "3/356117129.19" SPACECRAFT_CLOCK_STOP_COUNT = "3/356117348.19" PRODUCER_ID = "SONC" PRODUCER_FULL_NAME = "SCIENCE OPERATIONS AND NAVIGATION CENTER" PRODUCER_INSTITUTION_NAME = "CNES" INSTRUMENT_ID = SESAME INSTRUMENT_NAME = "SURFACE ELECTRIC SOUNDING AND ACOUSTIC MONITORING EXPERIMENT" INSTRUMENT_TYPE = {"ACOUSTIC SENSOR", "DUST IMPACT DETECTOR", "PERMITTIVITY PROBE"} TARGET_NAME = "CALIBRATION" TARGET_TYPE = "CALIBRATION" PROCESSING_LEVEL_ID = "2" DATA_QUALITY_ID = "-1" DATA_QUALITY_DESC = "-1 : NOT QUALIFIED" /* GEOMETRY PARAMETERS */ /* SPACECRAFT LOCATION: Position */ SC_SUN_POSITION_VECTOR = ( -105564281.5, 537375104.7, 297313863.8) /* TARGET PARAMETERS: Position , Velocity */ SC_TARGET_POSITION_VECTOR = ( -1247799.0, -3080843.8, -784682.2) SC_TARGET_VELOCITY_VECTOR = ( 288.724,701.459,172.574) /* SPACECRAFT POSITION WITH RESPECT TO CENTRAL BODY */ SPACECRAFT_ALTITUDE = 3415305.6 SUB_SPACECRAFT_LATITUDE = -13.41 SUB_SPACECRAFT_LONGITUDE = 180.28 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 = NT_TABLE NAME = "NT" INTERCHANGE_FORMAT = ASCII ROWS = 3 COLUMNS = 4 ROW_BYTES = 49 ^STRUCTURE = "DIM_NT.FMT" END_OBJECT = NT_TABLE END