PDS_VERSION_ID               = PDS3
LABEL_REVISION_NOTE  = "2017-03-02, SONC, version 1.0"
/* PVV version 3.13 */

/* Edited SC data from DIM Sensor Test Mode (SONC Level 2) */

RECORD_TYPE = FIXED_LENGTH
FILE_RECORDS = 2
RECORD_BYTES  = 79
FILE_NAME = "SES_FS2_DST_1411131337_Z.TAB"

/* DATA OBJECT POINTERS  */

^ST_TABLE = ("SES_FS2_DST_1411131337_Z.TAB",1 <BYTES>)

DATA_SET_ID           = "RL-C-SESAME-2-FSS-V1.0"
DATA_SET_NAME         = "ROSETTA-LANDER 67P SESAME 2 FSS V1.0"
PRODUCT_ID            = "SES_FS2_DST_1411131337_Z"
PRODUCT_CREATION_TIME = 2017-03-02T09:13:15
MISSION_NAME           = "INTERNATIONAL ROSETTA MISSION"
MISSION_PHASE_NAME    = "FIRST SCIENCE SEQUENCE"
MISSION_ID             = ROSETTA
INSTRUMENT_HOST_NAME   = "ROSETTA-LANDER"
INSTRUMENT_HOST_ID     = RL

PRODUCT_TYPE          = EDR
START_TIME            = 2014-11-13T13:37:31.993
STOP_TIME             = 2014-11-13T13:38:51.462
SPACECRAFT_CLOCK_START_COUNT = "3/374506580.24"
SPACECRAFT_CLOCK_STOP_COUNT  = "3/374506660.07"

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           = "67P/CHURYUMOV-GERASIMENKO 1 (1969 R1)"
TARGET_TYPE           = "COMET"

PROCESSING_LEVEL_ID   = "2"
DATA_QUALITY_ID        = "-1"
DATA_QUALITY_DESC      = "-1 : NOT QUALIFIED"

/* GEOMETRY PARAMETERS */

/* SPACECRAFT LOCATION: Position <km> */
SC_SUN_POSITION_VECTOR = ( -242971930.4, 319358584.0, 195552522.6)
/* TARGET PARAMETERS: Position <km>, Velocity <m/s> */
SC_TARGET_POSITION_VECTOR = (         16.6,        10.7,       -17.7)
SC_TARGET_VELOCITY_VECTOR = (  0.066, 0.414,-0.231)
/* SPACECRAFT POSITION WITH RESPECT TO CENTRAL BODY */
SPACECRAFT_ALTITUDE =          24.5 <km>
SUB_SPACECRAFT_LATITUDE =   -11.82 <deg>
SUB_SPACECRAFT_LONGITUDE =    35.80 <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               = ST_TABLE
   NAME               = "ST"
   INTERCHANGE_FORMAT = ASCII
   ROWS               = 2
   COLUMNS            = 11
   ROW_BYTES          = 79
   ^STRUCTURE         = "DIM_ST.FMT"
END_OBJECT           = ST_TABLE



END