******************************************************************** UARS WEEKLY STATUS REPORT - 07 SEP 2001 ******************************************************************** *********** SOLSTICE *********** Nothing received. *********** SUSIM *********** SUSIM has completed its daily solar scans this past week during periods of predicted UARS telemetry. As requested, we are verifying NRT files built on the PACOR-A system versus the CDHF versions. We are building our final calibrations to be used for reprocessing the latest level 1 data to level 3 at NRL. *********** ACRIM *********** Nothing received. *********** PEM *********** ***** ALL PEM COMMUNICATION SHOULD NOW BE THROUGH THE PEM2K:: NODE ***** PEM is saddened by the shutdown of UARS and appreciates all of the efforts of GSFC in the past and present of UARS. At the present time, PEM energy deposition from its spectrometers is not being generated. Recent data configuration changes have affected PEM software causing multiple failures. These failures are being reviewed by the PEM team. In order to correct for new telemetry requirements, PEM will need to update processing code with a patch delivery. The delivery patch may include changes which would allow the PEM software to execute on a DEC Alpha machine. GSFC is helping PEM with some DEC Alpha particulars which have caused PEM level 3 code to fail on DEC Alpha machines (software below level 3 executes on the DEC Alpha). Currently, PEM has requested GSFC assistance with compiling for the DEC Alpha since the GSFC executables run on the Alpha and SwRI's compiled versions do not. Updated HEPS calibration parameters have been finalized and are ready for delivery. Updated MEPS quality calibration files have been finalized and are ready for delivery. Level 3 software errors, discovered by Dr. Dean Pesnell, have been fixed; his suggestions have been incorporated with in the PEM production code. Both updated HEPS and MEPS calibration data, along with the Level 3 code changes, will influence the in-situ energy deposition predictions, so new versions of PEM energy deposition Level 3 files will be generated. *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 *********** The MPG participated in the UARS Monthly Status Review Meeting on 05 September 2001. On 06 September 2001 the MPG participated in the weekly UARS Technical Team Meeting. This series of meetings is being held to discuss contingencies since it appears that FY 2002 funds will be insufficient to continue collection of science data by the UARS instruments. Processing of instrument Daily Activity Plans continues with no problems. *********** CDHF *********** Nothing received. *********** FOT *********** REPORTING PERIOD This report covers 25 August 2001 (Orbit 54421, GMT Day 237) through 31 August 2001 (Orbit 54525, GMT Day 243). 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 MLS 237/2224 54435 Power OFF HALOE 238/0012 54436 Power ON The beta angle ranged between the angles of 46.3 degrees to 39.6 degrees for this report period. The beta angle is now decreasing towards a minimum angle of 0 degrees on 11 September 2001 (DOY 254). 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 1.2 to 1.3 degrees C. Additional battery performance data for each battery on 24 August 2001 and 31 August 2001 are provided in Appendix D. The clock error ranged from Ð12.1 to 10.0 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 = 00 ¥ ALERTS = 00 The following real-time command sheets were executed for the listed operational element(s) during this report period (see Appendix A). ¥ FOT = 20 ¥ HALOE = 01 ¥ MLS = 01 UARS Anomaly Reports initiated during this report period are listed in Appendix E and summarized below. ¥ FOT = 02 Zero (0) Anomaly Report remained OPEN at the end of this report period (see Appendix E). TRANSPONDER FREQUENCIES: · Transponder A: 00/316 - 2287.496493 · Transponder B: 01/119 - 2287.499116 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 01/242 show the observatory data loss to be 303 hours, 09 minutes, 13.504 seconds. This shows a loss of 15.808 seconds since the last report period. This is a 0.39 percent data loss, which equals a 99.61 percent data capture for the mission. The increase of 15.808 seconds of data loss occurred over three (3) days: · 27.840 seconds on Day 236 due to a Data Hit · 22.208 seconds on Day 237 due to a Data Hit · 09.760 seconds on Day 238 due to a Data Hit OTHER SIGNIFICANT EVENTS UARS SATELLITE OPERATIONS The FOT continues to support and plan for the possible decommissioning of the UARS spacecraft. A 3-minute calibration burn has been scheduled for 06 September 2001. The time of the burn has been set for 1310 GMT during the 1302-1327 GMT event. This burn should give the FOT and FDF a good handle on the duty cycle and efficiency of the thrusters. All issues with FDF product deliveries have been worked out and next TuesdayÕs products should include pre and predicted post burn data. MEETINGS The UARS FOT attended a UARS Readiness Meeting on Monday, August 27, 2001. The UARS FOT attended a UARS FDF Meeting on Monday, August 27, 2001. The UARS FOT attended a UARS Technical Team Meeting on Thursday, August 30, 2001. FUTURE SIGNIFICANT EVENTS The next UARS Yaw slew is scheduled for 11 September 2001 (DOY 254). 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 31 August 2001 ORBIT AOS NO. SUBSYS REASON ----- --- --- ------ ------ 54435 237/2224 01-532 MLS Power OFF 54436 238/0012 01-533 HALOE Power ON 54438 238/0414 01-534 OBC Clk Adj fr 20.6 to 0.00 msec/day 54440 238/0654 01-535 NBTR D 238 NOOPS 54446 238/1716 01-535 NBTR D238 NOOPS 54447 238/1759 01-536 NBTR D239 NOOPS 54454 239/0557 01-536 NBTR D 239 NOOPS 54461 239/1716 01-536 NBTR D239 NOOPS 54462 239/1801 01-537 NBTR D240 NOOPS 54470 240/0656 01-537 NBTR D 240 NOOPS 54476 240/1620 01-538 OBC RELOAD RTS 1 54476 240/1717 01-537 NBTR D240 NOOPS 54478 240/1900 01-539 OBC Clk Adj fr 0.00 to 20.6 msec/day 54484 241/0559 01-540 NBTR Day 241 NOOPS 54492 241/1802 01-540 NBTR Day 241 NOOPS 54492 241/1802 01-541 NBTR Day 242 NOOPS 54498 242/0418 01-542 OBC Clk Adj fr 20.6 to 0.00 msec/day 54499 242/0600 01-541 NBTR Day 242 NOOPS 54506 242/1718 01-541 NBTR Day 242 NOOPS 54507 242/1802 01-543 NBTR Day 243 NOOPS 54515 243/0742 01-543 NBTR NOOPS D-243 54522 243/1802 01-544 NBTR NOOPS D-244 ___________________________________________________________________________ APPENDIX B OUT-OF-LIMITS & ALERTS OCCURRENCES Week ending 31 August 2001 The following Out-Of-Limits occurrences were detected: MNEMONIC STATE DESCRIPTION ORBITS -------- ----- ----------- ------ -None this report period The following ALERT occurrences were detected: MNEMONIC DESCRIPTION ORBITS -------- ----------- ------ -None this report period _______________________________________________________________________________ APPENDIX C CLOCK & SOLAR ARRAY RATE CORRECTIONS Week ending 31 August 2001 CLOCK DRIFT RATE ADJUSTMENTS ORBIT TIME CLOCK RATE CHANGE ----- ----- ----------------- 54438 238/0416 Clk Adj fr 20.6 to 0.00 msec/day 54478 240/1902 Clk Adj fr 0.00 to 20.6 msec/day 54498 242/0419 Clk Adj fr 20.6 to 0.00 msec/day _______________________________________________________________________________ APPENDIX D UARS BATTERY PERFORMANCE DATA Week ending 31 August 2001 24 August 2001 - GMT Day 236 Beta = 45.9 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 +728.0/+728.0 -3.05/-3.99 +0.0/+0.0 12.0 0.000 0.0 2 +11.2/-123.2 +5.15/+4.19 +26.0/-14.4 25.4 1.030 19.7 3 +22.4/-50.4 +4.51/+3.23 +25.6/-14.4 25.4 1.020 19.6 31 August 2001 - GMT Day 243 Beta = 39.6 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 +728.0/+728.0 -2.73/-3.99 +0.0/+0.0 12.0 0.000 0.0 2 +11.2/-89.6 +6.11/+4.83 +27.2/-15.2 24.2 1.030 21.4 3 +22.4/-56.0 +5.15/+3.87 +27.2/-15.2 24.0 1.020 21.1 V/T LEVEL CHANGES ORB# TIME LVL FR-TO ----- ---- --------- -no changes V/T 5 _______________________________________________________________________________ APPENDIX E UARS ANOMALY REPORTS Week ending 24 August 2001 NEW ANOMALY REPORTS GENERATED AR NO. SUBSYS ORBIT TIME TTR PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- 01-052 FOT 54424 237/0555 14171 Generic Drop Out 01-053 FOT 54494 241/2100 24026 Late Acq (4:33) ANOMALY CLOSURE INFORMATION RECEIVED AR NO. SUBSYS ORBIT TIME TTR PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- 01-045 FOT see list August 01 14170 Generic Late Acquisition 01-052 FOT 54424 237/0555 14171 Generic Drop Out 01-053 FOT 54494 241/2100 24026 Late Acq (4:33) ANOMALY INVESTIGATION REPORTS GENERATED AR NO. SUBSYS ORBIT TIME TTR PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- -None this report period OPEN ANOMALY REPORTS AR NO. SUBSYS ORBIT TIME TTR PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- -None this report period SEVNTFW01/33