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         = 80964

FILE_NAME            = "CN_T_2_150918T000156.TAB"


/* DATA OBJECT POINTERS  */

^CN_AUX_TABLE        = ("CN_T_2_150918T000156.TAB",1 <BYTES>)


/* 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_150918T000156"
PRODUCT_CREATION_TIME  = 2017-09-07T15:17:16
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           = 2015-09-18T00:01:56
STOP_TIME            = 2015-09-28T00:00:53
SPACECRAFT_CLOCK_START_COUNT = "1/401155238.03394"
SPACECRAFT_CLOCK_STOP_COUNT  = "1/402019174.03027"
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 <km> */
SC_SUN_POSITION_VECTOR = (   14191610.0,-173173145.5, -93462568.9)
/* TARGET PARAMETERS: Position <km>, Velocity <m/s> */
SC_TARGET_POSITION_VECTOR = (        176.8,       142.3,      -237.4)
SC_TARGET_VELOCITY_VECTOR = ( -0.568, 0.197,-0.390)
/* SPACECRAFT POSITION WITH RESPECT TO CENTRAL BODY */
SPACECRAFT_ALTITUDE =         326.3 <km>
SUB_SPACECRAFT_LATITUDE =   -11.58 <deg>
SUB_SPACECRAFT_LONGITUDE =   349.12 <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_<TARGET_NAME> frame.
       All values are computed for the time = START_TIME.
       Distances are given in <km> velocities in <m/s>, angles in <deg>"

/* DATA OBJECT DEFINITION  */


OBJECT             = CN_AUX_TABLE
  NAME               = "OCN_E_BOX_ANT_TEMP"
  INTERCHANGE_FORMAT = ASCII
  ROWS               = 80964
  ^STRUCTURE         = "CN_AUX.FMT"
  COLUMNS            = 7
  ROW_BYTES          = 141
END_OBJECT         = CN_AUX_TABLE

END