PDS_VERSION_ID               = PDS3
LABEL_REVISION_NOTE  = "2017-02-16, SONC, version 1.0"
/* PVV version 3.13 */

/* General sesame related data - RMES (SONC Level 3) */

RECORD_TYPE = FIXED_LENGTH
FILE_RECORDS = 1
RECORD_BYTES  = 137
FILE_NAME = "SES_FS3_S___1409162031_RMES.TAB"

/* DATA OBJECT POINTERS  */

^RMES_TABLE     = ("SES_FS3_S___1409162031_RMES.TAB",1 <BYTES>)

DATA_SET_ID           = "RL-CAL-SESAME-3-PDCS-V1.0"
DATA_SET_NAME         = "ROSETTA-LANDER CAL SESAME 3 PDCS V1.0"
PRODUCT_ID            = "SES_FS3_S___1409162031_RMES"
PRODUCT_CREATION_TIME = 2017-02-16T09:20:52
MISSION_NAME           = "INTERNATIONAL ROSETTA MISSION"
MISSION_PHASE_NAME    = "PRE DELIVERY CALIB SCIENCE"
MISSION_ID             = ROSETTA
INSTRUMENT_HOST_NAME   = "ROSETTA-LANDER"
INSTRUMENT_HOST_ID     = RL

PRODUCT_TYPE          = RDR
START_TIME            = 2014-09-16T20:31:06.006
STOP_TIME             = 2014-09-16T20:31:06.006
SPACECRAFT_CLOCK_START_COUNT = "3/369520196.13"
SPACECRAFT_CLOCK_STOP_COUNT  = "3/369520196.13"

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   = "3"
DATA_QUALITY_ID        = "-1"
DATA_QUALITY_DESC      = "-1 : NOT QUALIFIED"

/* GEOMETRY PARAMETERS */

/* SPACECRAFT LOCATION: Position <km> */
SC_SUN_POSITION_VECTOR = ( -211421245.8, 392139553.8, 230817304.6)
/* TARGET PARAMETERS: Position <km>, Velocity <m/s> */
SC_TARGET_POSITION_VECTOR = (         13.0,        -9.6,        23.8)
SC_TARGET_VELOCITY_VECTOR = (  0.086, 0.140, 0.012)
/* SPACECRAFT POSITION WITH RESPECT TO CENTRAL BODY */
SPACECRAFT_ALTITUDE =          27.0 <km>
SUB_SPACECRAFT_LATITUDE =    32.40 <deg>
SUB_SPACECRAFT_LONGITUDE =    10.59 <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               = RMES_TABLE
  NAME               = "RMES"
  INTERCHANGE_FORMAT = ASCII
  ROWS               = 1
  COLUMNS            = 5
  ROW_BYTES          = 137
  ^STRUCTURE         = "SESAME_RMES.FMT"
END_OBJECT           = RMES_TABLE



END