PDS_VERSION_ID = PDS3 PRODUCT_VERSION_ID = "9.0" RECORD_TYPE = STREAM ^TEXT = "MESS_RS_ANT.TXT" OBJECT = TEXT PUBLICATION_DATE = 2015-10-09 NOTE = "Antenna Configuration File" END_OBJECT = TEXT 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_ANT" PRODUCT_TYPE = ANT PRODUCER_ID = "JHUAPL" PRODUCT_CREATION_TIME = 2015-06-12 START_TIME = 2011-019T15:01:59 STOP_TIME = 2015-120T23:24:59 SPACECRAFT_CLOCK_START_COUNT = "1/203936073" SPACECRAFT_CLOCK_STOP_COUNT = "2/72759796" DESCRIPTION = " The antenna pointing file contains antenna configuration of the MESSENGER spacecraft. This file accumulates as more data become available. Each record in the file contains the following four fields. Line 1. Column headings: # Year and Date (UTC), MET, Downlink, Uplink. Remaining Lines: Five values separated by one or more spaces: - Ground-receipt time Year: UTC time formatted as YYYY: - Ground-receipt time Date: UTC time formatted as DOY:HH:MM:SS.MMM - Spacecraft time: mission elapsed time (encoded SCLK form) - Spacecraft antenna used for downlink transmissions, as one of these values: 0: Front Fanbeam 1: AFT LGA 2: Front LGA 3: Bank Fanbeam 4: FWD LGA 5: Back LGA 6: Front Phased Array 7: Back Phased Array 8: Hardware Error - Spacecraft antenna used to receive the uplink, as one of these values: 0: Front Fanbeam 1: AFT LGA 2: Front LGA 3: Bank Fanbeam 4: FWD LGA 5: Back LGA 6: Front Phased Array 7: Back Phased Array 8: Hardware Error " END