SXT REPORT FOR WEEKS 38 ; 12 Sep 1993 - 19 Sep 1993 GENERAL STATUS Another week of smooth operations. On Thursday, 16 Sep, the Skew gryo was tested. This is explained further in the report below. Solar activity remained at a relatively low level. PERSONNEL Many visitors were seen at ISAS last week as a result of the Kofu meeting the week before. By the end, most had returned to their homes in the States or Europe. Hugh Hudson is currently in the States until next week and Sam Freeland and Greg Slater will return to the States at the end of this week. I will also make a short trip to Calif starting tomorrow, and will return the middle of next week. T. Shimizu will act as the Chief Observer while I am away. Next week's report (for Week 39) will probably be combined with the report for the following week. SOLAR ACTIVITY Solar activity remained at a high A Goes level. One C flare occurred on 16 Sep, however, it occurred during spacecraft night. Two coordinated observing campaigns are being planned. The first is with the Norikura Observatory during 23-30 Oct, weather permitting. The scientific emphasis will be on plasma diagnostics. The Norikura contact is K. Ichimoto and H. Hara will be assisting the observations. The second is a bright point campaign begining on or 4 or 5 Oct. with Kitt Peak, organized by Karen Harvey. SCIENCE PROGRESS With the number of visitors, there were many opportunities for discussions. Ron Moore found a nice example of an erupting flare on 15 November 1991 (but different from the famous 15 Nov event) and made a short of video of this event for his talk at Mitaka. Hugh Hudson's goes_reducer program, that estimates temperatures and emission measures, was improved by Pat Bornmann to give uncertainty estimates on those parameters. Dominic Zarro and Lemen worked extensively on the BCS spectral synthesis and fitting software. The Thursday seminar included three speakers: C. Schrijver (Utrecht), R. Hammer (Freiburg), and T. Nakagawa (Sendai). SXT OPERATIONS The SXT operations went very smoothly this week and there were no significant problems to report. SPACECRAFT GYRO CHANGE The Y-gyro drift rate has been increasing since March 1993. The drift rate of all gyros at launch were approximately .1 deg/hour, but the Y-gyro drift rate is currently approximately 5 deg/hour. The drift rate is not increasing monotonically, but has sometimes increased and sometimes decreased over long periods (days to weeks). The drift rates of the X and Z-gyros have not changed since launch and both remain below 0.1 deg/hour. Despite its drift rate increase, the Y-gyro performance is still adequate for attitude control. On Thurs, 16 Sep, the NEC engineers turned on the S-gyro (skew) to measure its drift rate. This gyro was tested briefly two years ago during the post-launch check-out period, but has not been turned on since. The S-gyro drift rate was measured on Thurs to be 0.04 deg/hour, which was essentially its launch value. Because this rate is so much lower than the Y-gyro drift rate, it was decided that on Monday, 20 Sep, the spacecraft control would be switched from X-, Y-, Z-gyro's to X-, Z-, and S-gyro's. This was accomplished during today's KSC contacts, and T. Kosugi has confirmed that there is an improvement in spacecraft attitude control. It should be noted that the performance of the Y-gyro is adequate for attitude control and could be used in the future if there are problems with the X-, Z- or S- gyro's. Now that the S-gyro is being used for attitude control, we will have to modify the software for SXT image registration to use the correct transformation relations. James R. Lemen 20 Sep 1993