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- Path: sparky!uunet!news.larc.nasa.gov!zip.larc.nasa.gov!sdd
- From: sdd@zip.larc.nasa.gov (Steve Derry)
- Newsgroups: sci.space
- Subject: Re: Mars Observer Update - 11/13/92
- Date: 17 Nov 1992 19:15:24 GMT
- Organization: NASA Langley Research Center, Hampton, VA USA
- Lines: 21
- Distribution: world
- Message-ID: <1ebgccINNch7@rave.larc.nasa.gov>
- References: <1992Nov13.192046.22718@news.arc.nasa.gov>
- NNTP-Posting-Host: zip.larc.nasa.gov
- Keywords: Mars Observer, JPL
-
- In article <1992Nov13.192046.22718@news.arc.nasa.gov>, baalke@kelvin.jpl.nasa.gov (Ron Baalke) writes:
- |>
- |> A new Star Catalog/Ephemeris was uplinked and a successful "USE"
- |> command radiated this morning. The ephemeris previously used had the
- |> intended effect of altering the solar array sun incidence angle by 5
- |> degrees, from 60 degrees to 55 degrees. This sun incidence angle periodic
- |> decrease will be performed in subsequent ephemeris loads, with the final
- |> objective being to point the high-gain antenna at earth by the time
- |> transition from inner to outer cruise takes place. The current offset is
- |> designed to prevent direct sunlight on the solar panels creating an excess
- |> amount of power. At the time of transition from inner to outer cruise, the
- |> spacecraft will be of sufficient distance from the sun that excess power
- |> is of a lesser concern.
-
- I understand why it is undesirable to point the solar array directly at the
- sun at this point in the mission. But why can't the HGA be pointed at earth?
- Aren't the solar array and HGA independedtly steerable?
-
- --
- Steve Derry
- <s.d.derry@larc.nasa.gov>
-