PDS_VERSION_ID               = PDS3
LABEL_REVISION_NOTE  = "2017-12-07, 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         = 21072

FILE_NAME            = "CN_T_2_041006T000118.DAT"


/* DATA OBJECT POINTERS  */

^CN_AUX_TABLE        = ("CN_T_2_041006T000118.TAB",1 <BYTES>)


/* IDENTIFICATION KEYWORDS */
DATA_SET_ID     = "RO/RL-CAL-CONSERT-2-CVP2-V1.0"
DATA_SET_NAME   = "ROSETTA-ORBITER/ROSETTA-LANDER CAL CONSERT 2 CVP2 V1.0"
PRODUCT_ID      = "CN_T_2_041006T000118"
PRODUCT_CREATION_TIME  = 2017-12-07T14:07:26
MISSION_NAME           = "INTERNATIONAL ROSETTA MISSION"
MISSION_ID             = ROSETTA
INSTRUMENT_HOST_NAME   = "ROSETTA-ORBITER"
INSTRUMENT_HOST_ID     = "RO"
OBSERVATION_TYPE    = "COMMISSIONING"

MISSION_PHASE_NAME     = "COMMISSIONING"
PRODUCT_TYPE         = EDR

START_TIME           = 2004-10-06T00:01:18
STOP_TIME            = 2004-10-15T23:57:02
SPACECRAFT_CLOCK_START_COUNT = " 1/55641661.03204"
SPACECRAFT_CLOCK_STOP_COUNT  = " 1/56505405.03217"
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         = "CALIBRATION"
TARGET_TYPE         = "CALIBRATION"


PROCESSING_LEVEL_ID = "2"
DATA_QUALITY_ID   = "N/A"
DATA_QUALITY_DESC = "N/A"

/* GEOMETRY PARAMETERS */

/* SPACECRAFT LOCATION: Position <km> */
SC_SUN_POSITION_VECTOR = ( -127017580.0, -92607882.8, -39112218.2)
/* TARGET PARAMETERS: Position <km>, Velocity <km/s> */
SC_TARGET_POSITION_VECTOR = ("N/A", "N/A", "N/A")
SC_TARGET_VELOCITY_VECTOR = ("N/A", "N/A", "N/A")
/* SPACECRAFT POSITION WITH RESPECT TO CENTRAL BODY */
SPACECRAFT_ALTITUDE =  "N/A"
SUB_SPACECRAFT_LATITUDE =  "N/A"
SUB_SPACECRAFT_LONGITUDE =  "N/A"
NOTE = "The values of the keyword SC_SUN_POSITION_VECTOR,
       are related to the equatorial J2000 inertial frame (EMEJ200).
       The values are computed for the time = START_TIME.
       Distances are given in <km>"



/* DATA OBJECT DEFINITION  */


OBJECT             = CN_AUX_TABLE
  NAME               = "E_BOX_ANT_TEMP"
  INTERCHANGE_FORMAT = ASCII
  ROWS               = 21072
  ^STRUCTURE         = "CN_AUX.FMT"
  COLUMNS            = 7
  ROW_BYTES          = 141
END_OBJECT         = CN_AUX_TABLE

END