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 ------------------------------------------------------------------------------- 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 ------------------------------------------------------------------------------