SETI public: Status Report for Voyager 1-2 for August 1, 2003

From: LARRY KLAES (ljk4_at_msn.com)
Date: Wed Sep 10 2003 - 11:48:01 PDT

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    http://voyager.jpl.nasa.gov/mission/weekly-reports/index.htm

    Voyager Mission Operations Status Report # 2003-08-01, Week Ending August 01, 2003
    Command Transmission & Verification Operations
    Voyager 1 command operations consisted of the uplink of a command loss timer reset on 07/29 [DOY 210/2315z]. The spacecraft received the command
    There were no Voyager 2 command operations during the period.
    Sequence Generation Operations
    Complete sequence development of CCSL B121.
    Data Return Operations
    Voyager 1 Data Processing and Operations:
    There were 91.1 hours of DSN scheduled support for Voyager 1 of which 35.3 hours were large aperture coverage. There were no real-time or schedule support changes made during the period.
    There was one significant outages of 0.7 hours duration on 07/26 [DOY 207] due to a power failure at SPC-10/DSS-14 [DR G103087].
    Science instrument performance was nominal for all activities during this period. One frame of GS-4 data was recorded this week. The AHELI1 cyclic for recording additional GS-4 data was enabled on November 17, 2001. A frame from this cyclic was recorded on August 1. The EDR backlog is 9 days.
    Voyager 2 Data Processing and Operations:
    There were 62.6 hours of DSN scheduled support for Voyager 2 of which 6.9 hours were large aperture coverage. There were no real-time or schedule support changes made or significant outages during the period.
    Science instrument performance was nominal for all activities during this period. One frame of GS-4 data was recorded on July 29. The EDR backlog is 9 days.
    Flight System Performance
    Voyager 1 performance was nominal during this report period. Activities included turning OFF the Azimuth Coil Heat on 7/29 (DOY 210) and turning ON Gyros A/B on 8/1 (DOY 213).
    Voyager 2 performance was nominal during this report period. Activity included a PMPCAL on 7/29 (DOY 210).
    PROPELLANT/POWER CONSUMABLES STATUS AS OF 7-31-03/8-01-03
    SpacecraftConsumption
    One Week (Gm)Propellant
    Remaining (Kg)Output
    (Watts)Margin
    (Watts)
    17.1530.02303.228
    26.9231.82304.753

    RANGE, VELOCITY AND ROUND TRIP LIGHT TIME AS OF 8/1/03
      Voyager 1Voyager 2
    Distance from the Sun (Km)13,325,000,00010,603,000,000
    Distance from the Sun (Mi)8,280,000,0006,588,000,000
    Distance from the Earth (Km)13,257,000,00010,479,000,000
    Distance from the Earth (Mi)8,237,000,0006,511,000,000
    Total Distance Traveled Since Launch (Km)15,149,000,00014,197,000,000
    Total Distance Traveled Since Launch (Mi)9,413,000,0008,821,000,000
    Velocity Relative to Sun (Km/sec)17.20415.677
    Velocity Relative to Sun (Mi/hr)38,48335,069
    Velocity Relative to Earth (Km/sec)42.07135.643
    Velocity Relative to Earth (Mi/hr)94,11079,730
    Round Trip Light Time (hh:mm:ss)24:34:0219:25:12


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