PDS_VERSION_ID                =  PDS3
PRODUCT_VERSION_ID            =  "1.0"
RECORD_TYPE                   =  STREAM
^TEXT                         =  "MESS_RS_2015114_2015114_MPD.TXT"

/* Identification Data Elements */
INSTRUMENT_NAME               =  "RADIO SCIENCE SUBSYSTEM"
INSTRUMENT_ID                 =  "RSS"
TARGET_NAME                   =  "MERCURY"
DATA_SET_ID                   =  "MESS-V/H-RSS-1-EDR-RAWDATA-V1.0"
MISSION_NAME                  =  "MESSENGER"
INSTRUMENT_HOST_NAME          =  "MESSENGER"
INSTRUMENT_HOST_ID            =  "MESS"
PRODUCT_ID                    =  "MESS_RS_2015114_2015114_MPD"
PRODUCT_TYPE                  =  MPD
ORIGINAL_PRODUCT_ID           =  "ocm17_pds.mpdf"
PRODUCER_ID                   =  "JHUAPL"
MISSION_PHASE_NAME            =  "MERCURY ORBIT YEAR 5"
PRODUCT_CREATION_TIME         =  2015-153T15:42:53.993
DESCRIPTION                   =  "Associated maneuver:  OCM17_PDS"
START_TIME                    =  2015-114T17:22:47.054
STOP_TIME                     =  2015-114T17:22:47.054
SPACECRAFT_CLOCK_START_COUNT  =  "N/A"
SPACECRAFT_CLOCK_STOP_COUNT   =  "N/A"
OBJECT                        =  TEXT
  NOTE                          =  "Maneuver Performance Data File (MPDF).
  The MPDF is used in the maneuver design process to specify the flow rates,
  moment arms, and thrust magnitudes foreach spacecraft thruster.  This
  product is described in the Description of the Maneuver Performance Data
  File document (DOCUMENT/MPD_DESC.TXT)."
  PUBLICATION_DATE              =  2014-03-07
END_OBJECT                    =  TEXT

END