PDS_VERSION_ID               = PDS3
LABEL_REVISION_NOTE  = "2017-08-31, SONC, version 1.0"
/* PVV version 3.13 */

/* Edited SC data from PP Passive Mode (SONC Level 2) */

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_PPM_1411130810"
PRODUCT_CREATION_TIME = 2017-08-31T11:58:12
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            = 2014-11-13T08:10:28.554
STOP_TIME             = 2014-11-13T08:13:40.085
SPACECRAFT_CLOCK_START_COUNT = "3/374486957.10"
SPACECRAFT_CLOCK_STOP_COUNT  = "3/374487148.27"

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 = ( -242862825.9, 319667122.8, 195704666.8)
/* TARGET PARAMETERS: Position <km>, Velocity <m/s> */
SC_TARGET_POSITION_VECTOR = (         15.2,         2.5,       -13.0)
SC_TARGET_VELOCITY_VECTOR = (  0.083, 0.420,-0.248)
/* SPACECRAFT POSITION WITH RESPECT TO CENTRAL BODY */
SPACECRAFT_ALTITUDE =          18.4 <km>
SUB_SPACECRAFT_LATITUDE =   -15.40 <deg>
SUB_SPACECRAFT_LONGITUDE =   271.06 <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                        = FILE
   RECORD_TYPE                   = FIXED_LENGTH
   RECORD_BYTES                  = 99
   FILE_RECORDS                  = 2
   ^PM_PAR_TABLE                  = "SES_FS2_PPM_1411130810_PAR.TAB"
   OBJECT               = PM_PAR_TABLE
      NAME               = "PM_PAR"
      INTERCHANGE_FORMAT = ASCII
      ROWS               = 2
      COLUMNS            = 11
      ROW_BYTES          = 99
      ^STRUCTURE         = "PP_PM2_PAR.FMT"
   END_OBJECT           = PM_PAR_TABLE
END_OBJECT                  = FILE

OBJECT                        = FILE
   RECORD_TYPE                   = FIXED_LENGTH
   RECORD_BYTES                  = 62
   FILE_RECORDS                  = 20
   ^PM_POW_TABLE                  = "SES_FS2_PPM_1411130810_POW.TAB"
   OBJECT               = PM_POW_TABLE
      NAME               = "PM_POW"
      INTERCHANGE_FORMAT = ASCII
      ROWS               = 20
      COLUMNS            = 5
      ROW_BYTES          = 62
      ^STRUCTURE         = "PP_PM2_POW.FMT"
   END_OBJECT           = PM_POW_TABLE
END_OBJECT                  = FILE



END