******************************************************************** UARS WEEKLY STATUS REPORT - 31 DEC 1999 ******************************************************************** *********** SOLSTICE *********** We continue to gather enough data to meet all the SOLSTICE science objectives during this period of reduced tape recorder operations. SOLSTICE operates normally, collecting solar data on all available orbital tracking periods and stellar calibration observations, whenever possible. *********** SUSIM *********** Nothing received. *********** ACRIM *********** Nothing received. *********** PEM *********** The PEM team wishes everyone Happy Holidays! Daily activity plans for the PEM instrument were successfully generated for the first two weeks of 2000. PEM health and safety data monitoring, which was reconfigured for day light operation, are being reviewed to determine if they can be modified to account for telemetry dropouts caused by the tape recorder failure. The PEM:: microVAX needs replacement as it is not Y2K compliant. 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. *********** CDHF *********** The CDHF continues to notify all PI Software Representatives when Data Gaps occur in the LEVEL0 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. 21 days GPI (4.05) PROD (CLAES L3B) (432R-419C-4F=9L) 41 days WIN (5.11A) PROD (L1-L3) (520R-230C-8F=282L) UARS CDHF REHOST: - SUSIM has successfully validated the output products created on the Rehost System from the SUSIM V7.1 testing. - Testing HRDI V4.4 on the Rehost System. - Testing SOLSTICE V4.62 on the Rehost System. DAAC DATA Data created in the month of October 1999 for HALOE, NMC, UKMO, and PEM has been loaded into the DAAC Transfer Tables. DAAC has been notified. CDHF pending software upgrades: none *********** FOT *********** REPORTING PERIOD This report covers 18 December, 1999 (Orbit 45185, GMT Day 352) through 24 December 1999 (Orbit 45289, GMT Day 358). SPACECRAFT OPERATION The observatory is now in Forward Flight (Southern Hemisphere viewing) and is performing nominally under two-battery operations. The instrument operational changes were: INSTRUMENT OPERATIONAL CHANGES Instrument Time Orbit Comment WINDII 357/2346 45274 Off The beta angle ranged between the angles of 26.8 degrees to 33.2 degrees for this report period. The beta angle is now decreasing toward a minimum angle of +1.0 degrees on 06 January 1999 (DOY 006). 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 17 December 1999 and 20 December 1999 are provided in Appendix D. The clock error ranged from -12.3 to 10.2 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. % OUT-OF-LIMITS = 05 % ALERTS = 00 The following real-time command sheets were executed for the listed operational element(s) during this report period (see Appendix A). % FOT = 13 % WINDII = 01 UARS Anomaly Reports initiated during this report period are listed in Appendix E and summarized below. % FOT = 06 Three (3) Anomaly Reports remained OPEN at the end of this report period (see Appendix E). TRANSPONDER FREQUENCIES: % Transponder A: 99/320 - 2287.496800 % Transponder B: 99/334 - 2287.499196 GROUND SYSTEM OPERATION Three (6) 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 99/357 show the observatory data loss to be 404 hours, 03 minutes, 40.729 seconds (an increase of 61 hours 55 minutes 32.000 seconds since the last report period). This is a 0.5586 percent data loss which equals a 99.4414 percent data capture for the mission. The increase of 61 hours 55 minutes 32.000 seconds occurred over seven (7) days: - 04 hours 34 minutes 58.688 seconds on Day 351 due to a S/C TR problem. - 05 hours 45 minutes 37.248 seconds on Day 352 due to a S/C TR problem. - 11 hours 30 minutes 11.072 seconds on Day 353 due to a S/C TR problem. - 10 hours 01 minutes 24.448 seconds on Day 354 due to a S/C TR problem. - 09 hours 56 minutes 52.960 seconds on Day 355 due to a S/C TR problem. - 10 hours 10 minutes 50.176 seconds on Day 356 due to a S/C TR problem. - 09 hours 55 minutes 37.408 seconds on Day 357 due to a S/C TR problem. OTHER SIGNIFICANT EVENTS UARS SATELLITE OPERATIONS UARS completed a nominal 0.4 degree roll maneuver to return to normal pointing. This finished up a request from WINDII for their science observations. This return maneuver was completed Thursday, December 23, 1999 at 18:26:13 Z. The FOT investigated a repeating low limit violation of the Communication and Data Handling current. A low current alert was flaging during random spacecraft contacts. After careful review it was determined that the low current limit violation was a result of the new tape recorder operations. The tape recorder draws more current depending on which state it is in, either playback, record or standby. More specifically, the tape recorder is in the standby mode during these low limit violations which consequently draws the least amount of current. Previously the recorder was either in playback mode or recorder thus never violating the low current limit. An action has been generated to lower the CDH current limit set to compensate for the new tape recorder management. The FOT developed a tape recorder management plan. This plan will be submitted for approval next week. 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 The FOT did not attend any meetings during this report period. 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. 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 January 6, 2000. This maneuver will be a Forward to Reverse Flight maneuver (Northern 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 24 December 1999 ORBIT AOS NO. SUBSYS REASON ----- --- --- ------ ------- 45198 352/2139 99-421 NBTR NOOPS 45213 353/2142 99-422 NBTR NBTR NOOPS 45228 354/2226 99-423 NBTR NBTR NOOPS 45239 355/1506 99-424 OBC Clk Adj fr 0.00 to 20.6 msec/day 45241 355/1826 99-425 NBTR NBTR RTS-58 45243 355/2149 99-426 NBTR NBTR NOOPS 45258 356/2051 99-427 NBTR NBTR NOOPS 45264 357/0712 99-427 NBTR NBTR NOOPS 45261 357/0310 99-428 OBC Clk Adj fr 20.6 to 0.00 msec/day 45270 357/1651 99-429 OBC Roll Maneuver 45272 357/2053 99-430 NBTR NBTR NOOPS 45274 357/2346 99-431 WINDII Power OFF 45285 358/1736 99-430 NBTR NBTR NOOPS 45286 358/1916 99-432 NBTR NBTR NOOPS ___________________________________________________________________________ APPENDIX B OUT-OF-LIMITS & ALERTS OCCURRENCES Week ending 24 December 1999 The following Out-Of-Limits occurrences were detected: MNEMONIC STATE DESCRIPTION ORBITS --------- ----- ------------ ------ HRPTSPBIMON R-LO PTS Pulse Bus Current Mon 45242 PWICDH Y-LO CDH CURRENT 45242-46,56 PWICDH Y-LO CDH Current 45269 PWICDH Y-LO CDH CURRENT 45276,7,8 HRPTSPBIMON Y-HI PTS Pulse Bus Current Mon 45282-6 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 24 December 1999 CLOCK DRIFT RATE ADJUSTMENTS ORBIT TIME CLOCK RATE CHANGE ----- ---- ----------------- 45239 355/15:11 (21 Dec 99) from 0.00 to 20.6 msec/day 45261 357/03:13 (23 Dec 99) from 20.6 to 0.00 msec/day _______________________________________________________________________________ APPENDIX D UARS BATTERY PERFORMANCE DATA Week ending 20 December 1999 17 Dec 1999 - GMT Day 351 Beta = 26.8 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 -44.8/-67.2 -2.73/-3.68 +0.0/+0.0 16.2 0.000 0.0 2 +39.2/-44.8 +7.09/+5.47 +31.2/-15.2 24.5 1.030 21.1 3 +33.6/-16.8 +5.79/+4.51 +30.8/-16.4 24.3 1.023 21.0 20 Dec 1999 - GMT Day 354 Beta = 31.8 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 -44.8/-67.2 -3.05/-3.99 +0.0/+0.0 16.2 0.000 0.0 2 +22.4/-44.8 +6.11/+5.15 +30.4/-15.2 24.8 1.030 21.5 3 +44.8/-11.2 +5.15/+3.87 +29.6/-16.0 24.8 1.028 21.3 V/T LEVEL CHANGES ORB# TIME LVL FR-TO ----- ------ ---------- no changes V/T 5 APPENDIX E UARS ANOMALY REPORTS Week ending 24 December 1999 NEW ANOMALY REPORTS GENERATED AR NO. SUBSYS ORBIT TIME TTR PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- 99-089 FOT 45188 352/0516 14170 Generic Late Acquisition 99-091 FOT 45190 352/0938 21717 Fwd link failure at WS 99-092 FOT 45226 354/1823 N/A AP 8 Crashed 99-093 FOT 45256 356/1911 21745 White Sands S/W prob 99-095 FOT 45273 357/2157 N/A AP2 Crash 99-096 FOT 45287 358/2015 21757 CSC Bad TDRSS Vectors ANOMALY CLOSURE INFORMATION RECEIVED AR NO. SUBSYS ORBIT TIME TTR PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- 99-091 FOT 45190 352/0938 21717 Fwd link failure at WS 99-092 FOT 45226 354/1823 N/A AP 8 Crashed 99-093 FOT 45256 356/1911 21745 White Sands S/W prob 99-095 FOT 45273 357/2157 N/A AP2 Crash 99-096 FOT 45287 358/2015 21757 CSC Bad TDRSS Vectors 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 99-089 FOT 45095 346/0123 14170 Generic Late Acquisition SEVNTFW99/52