Number 18 January 2002
Contents:
1) Update on FUSE status
Dear Colleagues,
As many recipients of this newsletter already know, FUSE science operations
were suspended on December 10, 2001, due to problems with two of the reaction
wheel assemblies on the spacecraft. The satellite is in a safe configuration
with solar arrays toward the sun, telescope doors closed, and detectors off.
The FUSE project is aggressively pursuing several avenues to enable us to return
FUSE to science as soon as possible. We are testing new ways of providing
three-axis attitude control of the satellite in the event one of the failed
wheels cannot be restarted. On December 20 a modification to the flight
software was installed that reestablished coarse three-axis control using the
two wheels plus magnetic torquer bars. The pointing since then has been
relatively stable, but far from the accuracy needed for science operations.
The doors will be reopened once the capability to reliably execute slews is
demonstrated. A new program to attempt to restart the y-axis wheel will begin
in the next week or two. Recent progress is very encouraging about the next
steps for reestablishing sufficient fine pointing control so that science
operations can be resumed in the near future.
FUSE uses reaction wheels to slew and maintain attitude. There are four wheels,
one in each of the three body axes and a fourth skew wheel that can
replace any of the other three. Two of the wheels, along the x and y axes, have
shown friction anomalies over the last two years, which caused short duration
(~1 day) erratic behavior and were autonomously shut down. However, engineers
from Orbital Sciences Corporation, the spacecraft manufacturer, were able to
restart the wheels with only a few days lost out of the science timeline.
On November 25th, the x-axis wheel stopped abruptly and several attempts to
restart it were unsuccessful. Science operations continued using the three
remaining operable wheels. On Monday December 10, the y-axis wheel stopped.
Although there has been a hint of wheel motion, it has not been possible to
spin up the wheel.
The new control mode uses the two operational reaction wheels in conjunction
with the satellite's magnetic torquer bars to provide control in all three axes.
The magnetic torquer bars are normally used to manage the momentum of the
reaction wheels by applying torques on the satellite against the earth's
magnetic field. The torques necessary to make up for the failed wheel are in
addition to those required for momentum management. This is well within the
capability of the magnetic torquer bars. Modifications to the satellite's
flight software for fine pointing control are being designed and tested by
Orbital engineers. The new flight code will be uplinked and tested with FUSE
in the near future.
The FUSE mission was at the peak of its scientific productivity when this
failure occurred. Over 50 papers based on FUSE observations will be presented
at the AAS meeting next week in Washington, DC. The FUSE Cycle 3 GI programs
were announced by NASA in October 2001. NASA intends to carry out the approved
GI and PI team observing programs, consistent with the capabilities and
constraints of the satellite.
We will continue to update you on the status of the satellite as the recovery
activities proceed.
Warren Moos
FUSE Principal Investigator
Johns Hopkins University
George Sonneborn
FUSE Project Scientist
NASA Goddard Space Flight Center
Hashima Hasan
FUSE Program Scientist
NASA Headquarters
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The Observer's Electronic Newsletter is published by the FUSE project and is
aimed at the FUSE user community.
Editor: B-G Andersson, Head FUSE User Support.
The FUSE Project is managed by Johns Hopkins University's Center for
Astrophysical Sciences in Baltimore, MD, for NASA's Goddard Space Flight
Center. The FUSE Principal Investigator is Dr. Warren Moos, the FUSE Project
Manager at JHU is Mr. J.B. Joyce, and the NASA Project Scientist for FUSE
is Dr. George Sonneborn.
Further information about the FUSE Guest Investigator Program can be
obtained from: Dr. George Sonneborn; sonneborn@stars.gsfc.nasa.gov
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