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 = 1
FILE_NAME = "SES_FS2_DNT_0808010607.TAB"

/* DATA OBJECT POINTERS  */

^NT_TABLE     = ("SES_FS2_DNT_0808010607.TAB",1 <BYTES>)

DATA_SET_ID           = "RL-CAL-SESAME-2-CR4A-V1.0"
DATA_SET_NAME         = "ROSETTA-LANDER CAL SESAME 2 CR4A V1.0"
PRODUCT_ID            = "SES_FS2_DNT_0808010607"
PRODUCT_CREATION_TIME = 2017-09-01T13:30:28
MISSION_NAME           = "INTERNATIONAL ROSETTA MISSION"
MISSION_PHASE_NAME    = "CRUISE 4-1"
MISSION_ID             = ROSETTA
INSTRUMENT_HOST_NAME   = "ROSETTA-LANDER"
INSTRUMENT_HOST_ID     = RL

PRODUCT_TYPE          = UDR
START_TIME            = 2008-08-01T06:07:42.548
STOP_TIME             = 2008-08-01T06:07:42.548
SPACECRAFT_CLOCK_START_COUNT = "2/176191625.17"
SPACECRAFT_CLOCK_STOP_COUNT  = "2/176191625.17"

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

/* GEOMETRY PARAMETERS */

/* SPACECRAFT LOCATION: Position <km> */
SC_SUN_POSITION_VECTOR = (  145838434.5, 241310594.2, 112628823.3)
/* 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 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               = 1
   COLUMNS            = 4
   ROW_BYTES          = 49
   ^STRUCTURE         = "DIM_NT.FMT"
END_OBJECT           = NT_TABLE



END