******************************************************************** UARS WEEKLY STATUS REPORT - 03 DEC 1999 ******************************************************************** *********** SOLSTICE *********** SOLSTICE continues to operate normally, collecting solar data on all available orbital tracking periods and stellar calibration observations, whenever possible. *********** SUSIM *********** In spite of continuing telemetry outages, the SUSIM was scheduled this past week for a normal set of solar scans. Although these were apparently successful, only about 75% of the data were retrieved. Potentially, this could raised to 100% if the times of telemetry availability are known at the time when SUSIM's plans are written. *********** ACRIM *********** Nothing received. *********** PEM *********** The PEM/AXIS was operated from November 22 through November 28. During this time, AXIS computed energy deposition from electrons which were derived from the measured X-ray spectrum. All 16 of the AXIS pixels were active. The PEM spectrometers continue to be active under PMON control*. While under PMON control, the PEM spectrometers computed energy deposition from electrons and protons measured in-situ by the particle spectrometers. *Beginning of power orbit day (PEM activation): array current >5 amps, array voltage >53.5 volts, and battery current >2.0 amps. End of power orbit day (PEM deactivation): time in power orbit day >4 minutes, array current <9 amps, and battery currents <0.2 amps. Power orbit day variation: ~39-40 min at yaw to ~50-51 min at maximum beta. *********** HALOE *********** Nothing received. *********** MLS *********** Nothing received. *********** HRDI *********** Nothing received. *********** WINDII *********** Nothing received. *********** MPG *********** Routine processing of instrument Daily Activity Plans continues with no problems. The MPG continues to assist the Project Scientist with the scheduling of instrument operations. The schedule of planned instrument operations for the next yaw cycle (8 December 1999 to 6 January 2000) was distributed. The MPG has continued to assist the FOT with analysis of the current tape recorder anomaly (NBTR B) and its impact on science data collection. *********** CDHF *********** The CDHF continues to notify all PI Software Representatives when Data Gaps occur in the LEVEL0 data due to the UARS Spacecraft Anomaly. The CDHF notified all PI Software Representatives regarding the re-ingest of UARS DAY 2998 Version 3 for better quality and more data. Appropriate production reprocessing was done against the Version 3 data. The CDHF processed current day data through level 3 for all active instruments. Additionally, CDHF personnel reprocessed: (R)= Requested (C) = Complete, (F)= Failed (L) = Days remaining to reprocess. 18 days CLA (7.0) PROD (L1-L3) (476R-418C-21F=37L) 15 days GPI (4.05) PROD (CLAES L3B) (372R-332C-2F=38L) 41 days WIN (5.11A) PROD (L1-L3) (520R-60C-4F=456L) UARS CDHF REHOST: - Testing SUSIM V7.1 on the Rehost System. - Preparing to test SOLSTICE V4.62 on the Rehost System. - Rehost procedures continued to be developed and/or reviewed. - Migration for all data levels continued. CDHF pending software upgrades: none *********** FOT *********** REPORTING PERIOD This report covers 20 November, 1999 (Orbit 44765, GMT Day 324) through 26 November 1999 (Orbit 44869, GMT Day 330). SPACECRAFT OPERATION The observatory is now in Reverse Flight (Northern Hemisphere viewing) and is performing nominally under two-battery operations. The instrument operational changes were: INSTRUMENT OPERATIONAL CHANGES Instrument Time Orbit Comment WINDII 326/0046 44795 On PEM 326/1214 44802 AXIS On HALOE 329/1714 44850 On WINDII 330/2312 44869 Off The beta angle ranged between the angles of 74.9 degrees to 50.3 degrees for this report period. The beta angle is now decreasing toward a minimum angle of -2.0 degrees on 08 December 1999 (DOY 342). Spacecraft battery 1, 2, and 3 performance monitoring continues. Battery 1 remains OFF the charge relay. Battery 2 and Battery 3 are currently maintaining greater than 23.8 V end-of-night (EON) load bus voltage. Battery temperatures are stable with a temperature delta between Battery 2 and Battery 3 of 1.0 to 1.3 degrees C. Additional battery performance data for each battery on 19 November 1999 and 26 November 1999 are provided in Appendix D. The clock error ranged from -11.4 to 11.4 msec during this report period. Clock rate adjustments are listed in Appendix C. All instrument and subsystem engineers were advised on the initial excursion of ALERTS or Out-Of-Limits conditions detected by the FOT for this report. A summary is listed below and the details of ALERT and Out-Of-Limits occurrences are listed in Appendix B. % ALERTS = 00 % OUT-OF-LIMITS = 11 The following real-time command sheets were executed for the listed operational element(s) during this report period (see Appendix A). % FOT = 07 % HRDI = 03 % WINDII = 02 % PEM = 01 % HALOE = 01 UARS Anomaly Reports initiated during this report period are listed in Appendix E and summarized below. % FOT = 02 Three (3) Anomaly Reports remained OPEN at the end of this report period (see Appendix E). TRANSPONDER FREQUENCIES: % Transponder A: 99/284 - 2287.496981 % Transponder B: 99/265 - 2287.498700 GROUND SYSTEM OPERATION Two (2) operational support problems occurred this period. Anomaly Reports are included in Appendix E. The data loss calculations supplied by Data Capture Facility (DCF) from mission start through UTC Day 99/329 show the observatory data loss to be 185 hours, 19 minutes, 46.873 seconds (an increase of 34 hours 22 minutes 56.768 seconds since the last report period). This is a 0.2587 percent data loss which equals a 99.7413 percent data capture for the mission. The increase of 34 hours 22 minutes 56.768 seconds occurred over seven (7) days: 7 00 hours 03 minutes 16.192 seconds on Day 323 due to a S/C TR problem. 7 00 hours 01 minutes 45.312 seconds on Day 324 due to a S/C TR problem. 7 00 hours 02 minutes 37.312 seconds on Day 325 due to a S/C TR problem. 7 05 hours 50 minutes 16.000 seconds on Day 326 due to a S/C TR problem. 7 11 hours 25 minutes 45.824 seconds on Day 327 due to a S/C TR problem. 7 08 hours 37 minutes 29.120 seconds on Day 328 due to a S/C TR problem. 7 08 hours 22 minutes 47.008 seconds on Day 329 due to a S/C TR problem. OTHER SIGNIFICANT EVENTS UARS SATELLITE OPERATIONS NBTR B anomalies continued again on Monday, Nov. 22, 1999. By Tuesday morning all PASS 1 data was non recoverable. NBTR B operation continued throughout the week with only PASS 2 data captured. Real-time supports were increased to compensate for the lost PASS 1 data. The current plan for NBTR B operations are the following: * Resume maximum coverage with a combination of TDRSS SSA and MA supports. * Continue NBTR B anomaly testing and analysis. * Continue NBTR B operations in 4-Mux mode. * Coordinate real-time supports with PASS 2 coverage. * Determine if PASS 2 and real-time operations can fulfill mission objectives. Currently only 56 to 62 minutes in a 96 minute orbit possible for real-time operations. * Review possibility of modification to UARS flight software and ground system to accept three TDRSS inputs to provide maximum orbital coverage. * Review science priorities with acquisition strategy to maximize science return. Initial science assessment by mid December. Final science review in early January. The Flight Operations Team completed the ERASE command test on Tuesday, Nov. 23, 1999. A /RAW command was used to send the Serial Magnitude command that was identified to the FOT to turn ERASE on. The FOT initiated this command in two forms, wind and erase as two separate commands and as a composite command. The ERASE function did not activate in either test scenario. To ensure that the ERASE did not activate even though telemetry showed the contrary, PASS 2 was recorded, dumped and evaluated. The PASS 2 data evaluated from this test was determined to be non-recoverable. YEAR 2000 OPERABILITY SUPPORT All areas identified to or by the Flight Operations Team for Y2K testing have been completed. There are no other areas identified at this time that have not been Y2K certified. MEETINGS No relevant meetings this week. FUTURE SIGNIFICANT EVENTS No specific date was agreed upon for UARS Safehold configuration discussions. Instead, the Supporting Engineers involved will be contacted every two weeks to determine if either the Flight Operations Team or Supporting Engineers have any new developments that should be discussed in a group. It is expected that one more meeting will be held before Y2k as an update to UARS safehold expectations for the new century. UARS has tested and prepared for the Year 2000 event. Special considerations have been made in preparation for a non nominal 1999 to 2000 transition. The next UARS Yaw slew is scheduled for December 8, 1999. This maneuver will be a Reverse to Forward Flight maneuver(Southern Hemisphere viewing). Attachments: Appendix A, Real-time Commands Sheets Appendix B, Out-Of-Limits & ALERT Occurrences Appendix C, Clock & Solar Array Rate Corrections Appendix D, UARS Battery Performance Data Appendix E, UARS Anomaly Reports APPENDIX A REAL-TIME COMMAND SHEETS Week ending 26 November 1999 ORBIT AOS NO. SUBSYS REASON ----- --- --- ------ ------- 44775 324/1610 99-388 HRDI SAFEHOLD DUE TO HIGH BARREL TEMP 44788 325/1240 99-389 HRDI SAFEHOLD DUE TO HIGH BARREL TEMP 44795 326/0046 99-390 WINDII POWER ON 44800 326/0734 99-377 HRDI SAFEHOLD DUE TO HIGH BARREL TEMP 44802 326/1214 99-391 OBC CLK ADJ. 41.2 to 20.6 MSEC/DAY 44802 326/1214 99-392 PEM AXIS ON 44809 326/2221 99-393 TMON DISA TMON 37 RPT 44821 327/1713 99-394 NBTR NBTR SPOOLING 44822 327/1858 99-395 NBTR NBTR FFWD ERASE 44825 328/0048 99-396 OBC TRANSMITTER NOOPS 44835 328/1627 99-397 OBC CLK ADJ. 20.6 to 41.2 MSEC/DAY 44850 329/1714 99-398 HALOE POWER ON 44858 330/0557 99-399 OBC CLK ADJ. 41.2 to 20.6 MSEC/DAY 44869 330/2312 99-400 WINDII POWER OFF __________________________________________________________________________ APPENDIX B OUT-OF-LIMITS & ALERTS OCCURRENCES Week ending 26 November 1999 The following Out-Of-Limits occurrences were detected: MNEMONIC STATE DESCRIPTION ORBITS --------- ----- ------------ ------ HRPTSBARTMP R-LO HRDI TELESCOPE BARREL TEMP 44768-75 HRPTSBARTMP Y-LO HRDI TELESCOPE BARREL TEMP 44776-7 HRPTSBARTMP Y-LO HRDI TELESCOPE BARREL TEMP 44783-86,89 HRPTSBARTMP R-LO HRDI TELESCOPE BARREL TEMP 44787-89 QTZEPSIF1 Y-LO ZEPS I/F PLATE AFT 44789-91 HRPTSBARTMP Y-LO HRDI TELESCOPE BARREL TEMP 44797,801 HRPTSBARTMP R-LO HRDI TELESCOPE BARREL TEMP 44798-800 HRPTSBARTMP Y-LO HRDI TELESCOPE BARREL TEMP 44815-24 HRPTSBARTMP R-LO HRDI TELESCOPE BARREL TEMP 44821 HRPTSBARTMP Y-LO HRDI TELESCOPE BARREL TEMP 44825-35 HRPTSPBIMON Y-HI HRDI Telescope Barrel 44847 The following ALERT occurrences were detected: MNEMONIC DESCRIPTION ORBITS --------- ------------ ------ No Alerts to report this report period. ______________________________________________________________________ APPENDIX C CLOCK & SOLAR ARRAY RATE CORRECTIONS Week ending 26 November 1999 CLOCK DRIFT RATE ADJUSTMENTS ORBIT TIME CLOCK RATE CHANGE ----- ---- ----------------- 44802 326/12:20 (22 Nov 99) from 41.2 to 20.6 msec/day 44835 328/16:30 (24 Nov 99) from 20.6 to 41.2 msec/day 44858 330/06:00 (26 Nov 99) from 41.2 to 20.6 msec/day ________________________________________________________________________ APPENDIX D UARS BATTERY PERFORMANCE DATA Week ending 26 November 1999 19 Nov 1999 - GMT Day 323 Beta = 74.9 deg, SA Pos = 269 deg DIFF V (mV) TEMP (C) CURR (amp) EON V AVE C/D AVE BAT MAX/MIN MAX/MIN MAX/MIN MIN RATIO DOD(%) --- ---------- ------- --------- ----- ------- ------ 1 -67.2/-89.6 -2.42/-3.36 +0.0/+0.0 16.3 0.000 0.0 2 +22.4/+0.0 +3.23/+1.66 +16.8/-14.8 27.5 1.037 13.4 3 +22.4/-22.4 +2.29/+1.34 +16.0/-14.4 27.4 1.035 12.9 26 Nov 1999 - GMT Day 330 Beta = 50.3 deg, SA Pos = 269 deg DIFF V (mV) TEMP (C) CURR (amp) EON V AVE C/D AVE BAT MAX/MIN MAX/MIN MAX/MIN MIN RATIO DOD(%) --- ---------- -------- --------- ----- ------- ------ 1 -56.0/-78.4 -3.68/-4.94 +0.0/+0.0 16.2 0.000 0.0 2 +84.0/+0.0 +5.47/+4.19 +28.4/-16.0 25.3 1.030 19.5 3 +22.4/-22.4 +4.51/+2.92 +27.2/-15.2 25.1 1.027 19.1 V/T LEVEL CHANGES ORB# TIME LVL FR-TO ----- --- ---------- no changes V/T 5 APPENDIX E UARS ANOMALY REPORTS Week ending 26 November 1999 NEW ANOMALY REPORTS GENERATED AR NO. SUBSYS ORBIT TIME TTR PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- 99-085 FOT 44810 327/0008 21603 512 kb playbacks errors 99-086 FOT 44823 327/2109 21606 TPF - No I channel 99-081 FOT 44843 329/0509 14170 Generic Late Acquisition ANOMALY CLOSURE INFORMATION RECEIVED AR NO. SUBSYS ORBIT TIME TTR PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- 99-085 FOT 44810 327/0008 21603 512 kb playbacks errors 99-086 FOT 44823 327/2109 21606 TPF - No I channel ANOMALY INVESTIGATION REPORTS GENERATED AR NO. SUBSYS ORBIT TIME TTR PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- No new reports generated OPEN ANOMALY REPORTS AR NO. SUBSYS ORBIT TIME TTR PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- 99-064 FOT 44135 10/8-9/99 N/A HRDI Cal Lamp Errors 99-071 FOT 44398 299/1212 21512 TPF Not Receiving 512 PB 99-081 FOT November 14170 Generic Late Acquisition SEVNTFW99/48