PDS_VERSION_ID               = PDS3
LABEL_REVISION_NOTE  = "2017-09-01, SONC, version 1.0"
/* PVV version 3.13 */

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

RECORD_TYPE = UNDEFINED
FILE_RECORDS = 2
FILE_NAME = "SES_FS2_DNT_0611281635.TAB"

/* DATA OBJECT POINTERS  */

^NT_TABLE     = ("SES_FS2_DNT_0611281635.TAB",1 <BYTES>)

DATA_SET_ID           = "RL-M-SESAME-2-MARS-V1.0"
DATA_SET_NAME         = "ROSETTA-LANDER MARS SESAME 2 MARS V1.0"
PRODUCT_ID            = "SES_FS2_DNT_0611281635"
PRODUCT_CREATION_TIME = 2017-09-01T07:53:43
MISSION_NAME           = "INTERNATIONAL ROSETTA MISSION"
MISSION_PHASE_NAME    = "MARS SWING-BY"
MISSION_ID             = ROSETTA
INSTRUMENT_HOST_NAME   = "ROSETTA-LANDER"
INSTRUMENT_HOST_ID     = RL

PRODUCT_TYPE          = UDR
START_TIME            = 2006-11-28T16:35:43.675
STOP_TIME             = 2006-11-28T16:44:43.862
SPACECRAFT_CLOCK_START_COUNT = "1/123352516.02"
SPACECRAFT_CLOCK_STOP_COUNT  = "1/123353056.08"

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           = "MARS"
TARGET_TYPE           = "PLANET"

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

/* GEOMETRY PARAMETERS */

/* SPACECRAFT LOCATION: Position <km> */
SC_SUN_POSITION_VECTOR = (  137429253.2,  79193435.6,  37610668.5)
/* TARGET PARAMETERS: Position <km>, Velocity <m/s> */
SC_TARGET_POSITION_VECTOR = (  -20471637.2, -78056134.7, -30249319.1)
SC_TARGET_VELOCITY_VECTOR = ( 7222.870,13602.922,5733.799)
/* SPACECRAFT POSITION WITH RESPECT TO CENTRAL BODY */
SPACECRAFT_ALTITUDE =    86175890.2 <km>
SUB_SPACECRAFT_LATITUDE =     1.01 <deg>
SUB_SPACECRAFT_LONGITUDE =    90.54 <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               = NT_TABLE
   NAME               = "NT"
   INTERCHANGE_FORMAT = ASCII
   ROWS               = 2
   COLUMNS            = 4
   ROW_BYTES          = 49
   ^STRUCTURE         = "DIM_NT.FMT"
END_OBJECT           = NT_TABLE



END