PDS_VERSION_ID = PDS3 LABEL_REVISION_NOTE = "2017-09-07, SONC, version 1.0" /* PVV version 3.13 */ /* Edited TCU data (Level 2) */ /* FILE CHARACTERISTIC DATA ELEMENTS */ RECORD_TYPE = FIXED_LENGTH RECORD_BYTES = 141 FILE_RECORDS = 80988 FILE_NAME = "CN_T_2_150620T000051.TAB" /* DATA OBJECT POINTERS */ ^CN_AUX_TABLE = ("CN_T_2_150620T000051.TAB",1 ) /* IDENTIFICATION KEYWORDS */ DATA_SET_ID = "RO/RL-C-CONSERT-2-LTS-V1.0" DATA_SET_NAME = "ROSETTA-ORBITER/ROSETTA-LANDER 67P CONSERT 2 LTS V1.0" PRODUCT_ID = "CN_T_2_150620T000051" PRODUCT_CREATION_TIME = 2017-09-07T15:11:57 MISSION_NAME = "INTERNATIONAL ROSETTA MISSION" MISSION_ID = ROSETTA INSTRUMENT_HOST_NAME = "ROSETTA-ORBITER" INSTRUMENT_HOST_ID = "RO" OBSERVATION_TYPE = "LONG TERM SCIENCE" MISSION_PHASE_NAME = "LONG TERM SCIENCE" PRODUCT_TYPE = EDR START_TIME = 2015-06-20T00:00:51 STOP_TIME = 2015-06-29T23:59:47 SPACECRAFT_CLOCK_START_COUNT = "1/393379174.03165" SPACECRAFT_CLOCK_STOP_COUNT = "1/394243110.04600" ORBIT_NUMBER ="N/A" PRODUCER_ID = "SONC" PRODUCER_FULL_NAME = "SCIENCE OPERATIONS AND NAVIGATION CENTER" PRODUCER_INSTITUTION_NAME = "CNES" INSTRUMENT_ID = CONSERT INSTRUMENT_NAME = "COMET NUCLEUS SOUNDING EXPERIMENT BY RADIOWAVE TRANSMISSION" INSTRUMENT_TYPE = "RADAR" INSTRUMENT_MODE_ID = "PINGPONG" INSTRUMENT_MODE_DESC = "CONSERT PERFORMS SOUNDING MEASUREMENTS AS A TRANSPONDER. CONSERT ORBITER AND CONSERT LANDER UNITS ARE SYNCHRONIZED." TARGET_NAME = "67P/CHURYUMOV-GERASIMENKO 1 (1969 R1)" TARGET_TYPE = "COMET" PROCESSING_LEVEL_ID = "2" DATA_QUALITY_ID = "N/A" DATA_QUALITY_DESC = "N/A" /* GEOMETRY PARAMETERS */ /* SPACECRAFT LOCATION: Position */ SC_SUN_POSITION_VECTOR = ( -199762146.1, -64534918.8, -12890574.3) /* TARGET PARAMETERS: Position , Velocity */ SC_TARGET_POSITION_VECTOR = ( 55.4, -173.5, 13.8) SC_TARGET_VELOCITY_VECTOR = ( -0.001,-0.099, 0.782) /* SPACECRAFT POSITION WITH RESPECT TO CENTRAL BODY */ SPACECRAFT_ALTITUDE = 180.6 SUB_SPACECRAFT_LATITUDE = -1.75 SUB_SPACECRAFT_LONGITUDE = 40.72 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 = CN_AUX_TABLE NAME = "OCN_E_BOX_ANT_TEMP" INTERCHANGE_FORMAT = ASCII ROWS = 80988 ^STRUCTURE = "CN_AUX.FMT" COLUMNS = 7 ROW_BYTES = 141 END_OBJECT = CN_AUX_TABLE END