PDS_VERSION_ID               = PDS3
LABEL_REVISION_NOTE  = "2016-12-05, SONC, version 1.0"
/* PVV version 3.13 */

/*          Edited Auxiliary Data (Level 2)         */


/* FILE CHARACTERISTIC DATA ELEMENTS */

RECORD_TYPE          = FIXED_LENGTH
RECORD_BYTES         = 55
FILE_RECORDS         = 30
FILE_NAME            = "PTO_FAX2_141113104104_0000.TAB"


/* DATA OBJECT POINTERS  */

^AUXILIARY_TABLE     = ("PTO_FAX2_141113104104_0000.TAB",1 <BYTES>)


DATA_SET_ID           = "RL-C-PTOLEMY-2-FSS-V1.0"
DATA_SET_NAME         = "ROSETTA-LANDER 67P PTOLEMY 2 FSS V1.0"
PRODUCT_ID            = "PTO_FAX2_141113104104_0000"
PRODUCT_CREATION_TIME = 2016-12-05T12:49:32
MISSION_NAME           = "INTERNATIONAL ROSETTA MISSION"
MISSION_PHASE_NAME    = "FIRST SCIENCE SEQUENCE"
MISSION_ID             = ROSETTA
INSTRUMENT_HOST_NAME   = "ROSETTA-LANDER"
INSTRUMENT_HOST_ID     = RL
OBSERVATION_TYPE    = "FIRST SCIENCE SEQUENCE"

PRODUCT_TYPE          = EDR
START_TIME            = 2014-11-13T10:41:04.177
STOP_TIME             = 2014-11-13T10:41:09.177
SPACECRAFT_CLOCK_START_COUNT = "3/0374495992.65"
SPACECRAFT_CLOCK_STOP_COUNT  = "3/0374495997.65"

PRODUCER_ID            = "SONC"
PRODUCER_FULL_NAME     = "SCIENCE OPERATIONS AND NAVIGATION CENTER"
PRODUCER_INSTITUTION_NAME = "CNES"

INSTRUMENT_ID          = PTOLEMY
INSTRUMENT_NAME        ="PTOLEMY - GAS CHROMATOGRAPH ISOTOPE RATIO
                         MASS SPECTROMETER"
INSTRUMENT_TYPE        = "GAS ISOTOPE RATIO ANALYSER"
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        = "0"
DATA_QUALITY_DESC      =  "0 : SEQUENCE PERMORMED AS EXPECTED"


/* GEOMETRY PARAMETERS */

/* SPACECRAFT LOCATION: Position <km> */
SC_SUN_POSITION_VECTOR = ( -242913080.4, 319525078.7, 195634625.8)
/* TARGET PARAMETERS: Position <km>, Velocity <m/s> */
SC_TARGET_POSITION_VECTOR = (         15.9,         6.3,       -15.2)
SC_TARGET_VELOCITY_VECTOR = (  0.074, 0.418,-0.239)
/* SPACECRAFT POSITION WITH RESPECT TO CENTRAL BODY */
SPACECRAFT_ALTITUDE =          20.8 <km>
SUB_SPACECRAFT_LATITUDE =   -10.78 <deg>
SUB_SPACECRAFT_LONGITUDE =   341.30 <deg>
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_67P/C-G frame.
       All values are computed for the time = START_TIME.
       Distances are given in <km> velocities in <m/s>, angles in <deg>"

/* 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               = AUXILIARY_TABLE
  NAME               = "AUXILIARY"
  INTERCHANGE_FORMAT = ASCII
  ROWS               = 30
  COLUMNS            = 4
  ROW_BYTES          = 55
  DESCRIPTION        = "PTOLEMY Auxiliary data"
  ^STRUCTURE         = "PTOLEMY_AX2.FMT"
END_OBJECT           = AUXILIARY_TABLE



END