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SLR-Mail No.1189

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Date:2004-02-20 00:24:00
Sender:Frank Lemoine <flemoine@santafe.gsfc.nasa.gov>
Subject:[SLR-Mail] No. 1189: GFO-1 tracking during upcoming full-sun orbit regime.
Author:Frank Lemoine
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SLR Electronic Mail 2004-02-20 00:24:00 UTC Message No. 1189
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Author: Frank Lemoine
Subject: GFO-1 tracking during upcoming full-sun orbit regime.


Dear colleagues,

This message is to advise that the GEOSAT Follow-On spacecraft
will suspend the collection of altimeter data, and enter
sun-acquistion mode from approximately February 22 to April 2,
2004. GFO will shortly enter a full-Sun regime, inducing abnormally
high temperatures in the spacecraft. It is believed the performance
of the momentum wheels degrades at high temperatures. To prevent the
loss of the spacecraft (which is now six years old!),
the payloads will be turned off and GFO will
be placed in a 2-wheel sun acquisition mode (solar arrays
perpendicular to the Sun using only the two ´good´ momentum wheels).
Flaky momentum wheel performance in the last full sun regime
during the autumn of 2003 was identified as the cause of the spacecraft entering
contingency mode.
In sun-acquistion mode, tracking will be possible only intermittently,
and we advise the stations to temporarily suspend tracking GFO.

As per our agreement with NOAA and the US Navy, we have agreed
to suspend delivery of the medium precision orbits over this time
period. Accordingly, the delivery of IRV predictions will also
be suspended.

We will resume IRV predictions based on the Doppler data
on approximately April 2.

We are fortunate that due to orbit geometry considerations,
the full-Sun regime to be experienced by GFO in the next month
will be the last time the spacecraft will face this problem
for several years. The next periods of face-on (high beta prime)
orbit geometry will occur at the equinoxes where eclipses will
occur at the high latitudes.

Please do not hesitate to contact us if you have
any questions or concerns. We will apprise the stations
and the ILRS of any change to the dates of GFO down time.

In our orbit group, we plan to use this down time in
the production of the medium precision orbits, to update
the models and procedures for the production of the
precise ephemerides (POE´s).

Thank you for your continued support of this mission.

Regards,
Frank Lemoine
Space Geodesy Branch, Code 926
NASA Goddard Space Flight Center

From: flemoine@santafe.gsfc.nasa.gov

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