******************************************************************** UARS WEEKLY STATUS REPORT - 28 JAN 2005 ******************************************************************** *********** SOLSTICE *********** SOLSTICE continues to perform nominally, taking solar data on all available orbital tracking periods. This week we received about 65% of each day's data amounting to nearly 486 minutes of solar observing time per day. *********** SUSIM *********** SUSIM successfully gathered daily mid (1.1 nm) resolution, MgII, occultation, solar pointing offset, and continuous monitoring scans for time periods with UARS telemetry or tape recording. *********** PEM *********** HEPSA data files are version 2. Currently, HEPSA data between 1991274 and 2004259 has been reprocessed and archived at the GSFC DAAC. HEPSA data between 2004260 and 2004269 are waiting archival at GSFC DAAC. MEPS data files are version 1. Processed MEPS data files at the DAAC archive are between 1991274 and 2004239. MEPS data between 2004240 and 2004259 are waiting for archival at the DAAC. MEPS data between 2004260 and 2004269 are currently being processed. PEM continues to receive NMC data files from NOAA. No problems have been encountered. The PEM data from the GUVI conjunction periods may be found at http://wwwpem.space.swri.edu/guvi-pem.html. The additional electron data for the October and November storms of 2003 has been moved and is now located at http://climatology.space.swri.edu/uars_fromRudy.html. For those users of SDDAS, update your UARS Meta data and these data times will appear with full functionality. Proton data from these storms are now located at http://climatology.space.swri.edu/UARS_images_from_Rudy_(Apr._2004).html Requests have been received for storm spectral data. Overview plots were produced and these plots may be found on the web at http://climatology.space.swri.edu/UARS_images_postedJune2004.html for the storms of October 29 of 1991, November 8-9 of 1991, April 6-7 of 2000, March 31 - April 1 of 2001, April 11-12 of 2001, November 6-7 of 2001, and November 11-12 of 2001. *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. *********** MPG *********** The MPG continues to serve as the point-of-contact for UARS instrument operations in support of the Science Traceability Mission of UARS. Daily processing of instrument Daily Activity Plans continues with no problems. *********** CDHF *********** Nothing received. *********** FOT *********** REPORTING PERIOD This report covers 15 January 2005 (Orbit 73045, GMT Day 015) through 21 January 2005 (Orbit 73150, GMT Day 021). 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 SOLSTICE 015/1406 73054 DAY ONLY TO FULLTIME SUSIM 015/1548 73055 POWER ON HALOE 017/1259 73083 POWER ON The beta angle ranged between the angles of 12.2 degrees to 30.7 degrees for this report period. The beta angle is now increasing towards a maximum angle of 39 degrees on 27 January 2005 (DOY 027). 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 23.6 V end-of-night (EON) load bus voltage. Battery temperatures are stable with a temperature delta between Battery 2 and Battery 3 of 0.65 to 1.00 degrees C. Additional battery performance data for each battery on 14 January 2005 and 21 January 2005 are provided in Appendix D. The clock error ranged from 10.1 to -10.1 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 = 03 The following real-time command sheets were executed for the listed operational element(s) during this report period (see Appendix A). FOT = 09 SOLSTICE = 01 SUSIM = 02 PEM = 01 HALOE = 02 UARS Anomaly Reports initiated during this report period are listed in Appendix E and summarized below. FOT = 05 Three (3) Anomaly Reports remained OPEN at the end of this report period (see Appendix E). GROUND SYSTEM OPERATION Two (2) operational support problems occurred this period. Anomaly Reports are included in Appendix E. The data loss calculations are no longer being supplied by Data Capture Facility (DCF). OTHER SIGNIFICANT EVENTS UARS SATELLITE OPERATIONS This week the FOT continued to closely monitor the batteries. On Monday afternoon the Battery-2 temperature broke 8 degrees for the second consecutive orbit, so the MPS was commanded back to VT-6. The battery differentials were nominal for the first several orbits after the change and then began to push the -300 mV level by the 018/1724 Z event. The FOT met with the NASA power branch engineer and decided the maximum differential allowable before going back to VT-7. That limit was exceeded on the 019/0852 event when the differential voltage on Battery-3 hit -459 mV. The MPS was then commanded back to the VT-7 charge rate. Since that time, the batteries have performed nominally and the MPS continues to utilize the VT-7 charge rate. The FOT also continued their CMS software acceptance testing this week. The goal for completion is no later than end of January 2005. MEETINGS The FOT met with the NASA power branch engineers on 19 January 2005 to discuss the short and long term plans to manage the UARS batteries. FUTURE SIGNIFICANT EVENTS The next UARS Yaw slew is scheduled for 12 February 2005 (DOY 043). This maneuver will be a Forward to Reverse Flight maneuver (Northern Hemisphere viewing). Attachments: Appendix A, Real-time Command 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 21 January 2005 ORBIT AOS NO. SUBSYS REASON ----- --- --- ------ ------ 73054 015/1406 05-017 SOLSTICE DAY ONLY TO FULLTIME OPS 73054 015/1406 05-015 PMON ACTION #23 RESET/ENABLE 73055 015/1548 05-018 SUSIM POWER ON - PART-1 START 73055 015/1627 05-018 SUSIM POWER ON - PART-1 COMPLETED 73060 015/2320 05-019 OBC/CLK CLK ADJ FR 0.0 TO -20.6 MSEC/DAY 73068 016/1223 05-020 PEM POWER ON - DAY ONLY 73068 016/1303 05-018 SUSIM POWER ON - PART TWO 73068 016/1313 05-021 SUSIM POWER ON - SUPPLEMENT (START) 73069 016/1337 05-021 SUSIM POWER ON - SUPPLEMENT (FINISH) 73079 017/0534 05-022 OBC/CLK CLK ADJ FR -20.6 TO 0.0 MSEC/DAY 73083 017/1259 05-023 HALOE POWER ON - PART 1 73086 017/1726 05-024 HALOE POWER ON - PART 2 73087 017/1948 05-025 MPS VT L-7 TO VT L-6 73088 017/2057 05-026 MPS BATSOC 73111 019/0852 05-027 MPS VT LEVEL 6 TO VT-7 73119 019/2231 05-028 MPS PMON ACTION CLEAR 73135 021/0007 05-029 MACS RE-ENABLE 4 WHEEL CONTROL APPENDIX B OUT-OF-LIMITS & ALERTS OCCURRENCES Week ending 21 January 2005 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 -------- ----------- ------ OBSPMACENA23 PMON ACTION 23 OOL 73100 OBSPMGPOOL31 PMON GROUP 31 OOL 73100 OBSRWY PITCH WHEEL FAIL 73134 APPENDIX C CLOCK & SOLAR ARRAY RATE CORRECTIONS Week ending 21 January 2005 CLOCK DRIFT RATE ADJUSTMENTS ORBIT TIME CLOCK RATE CHANGE ----- ----- ----------------- 73060 015/2328 CLK ADJ FR 0.0 TO -20.6 MSEC/DAY 73079 017/0534 CLK ADJ FR -20.6 TO 0.0 MSEC/DAY APPENDIX D UARS BATTERY PERFORMANCE DATA Week ending 21 January 2005 14 January 2005 - GMT Day 014 Beta = 08.3 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 -700.0/-700.0 -3.05/-4.31 +00.0/+00.0 07.0 0.00 0.0 2 67.2/ 00.0 +6.43/+4.82 +28.0/-12.8 26.4 1.03 18.9 3 -33.6/-313.6 +4.50/+2.91 +26.0/-11.2 26.4 1.04 17.5 21 January 2005 - GMT Day 021 Beta = 30.7 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 -700.0/-700.0 -3.05/-1.80 +00.0/+00.0 07.0 0.00 0.0 2 50.4/ -11.2 +9.39/+8.39 +28.4/-15.2 26.7 1.05 21.0 3 -00.0/-123.6 +7.08/+6.43 +26.4/-14.8 26.7 1.04 19.7 V/T LEVEL CHANGES ORB# AOS TIME LVL FR-TO ----- -------- --------- 73087 017/1948 LV7 -> LV6 73111 019/0852 LV6 -> LV7 APPENDIX E UARS ANOMALY REPORTS Week ending 21 January 2005 NEW ANOMALY REPORTS GENERATED AR NO. SUBSYS ORBIT TIME CDS PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- 05-001 FOT 73056 015/1807 30832 Generic Late Acquisition 05-001 FOT 73094 018/0525 30832 Generic Late Acquisition 05-003 MPS 73100 018/1538 N/A PMON GRP 31 AND ACTION 23 OOL 05-001 FOT 73124 020/0628 30832 Generic Late Acquisition 05-004 MACS 73134 020/2122 N/A Pitch Wheel Anomaly ANOMALY CLOSURE INFORMATION RECEIVED AR NO. SUBSYS ORBIT TIME CDS PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- -None this report period. ANOMALY INVESTIGATION REPORTS GENERATED AIR NO. SUBSYS ORBIT TIME CDS PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- -None this report period. OPEN ANOMALY REPORTS AR NO. SUBSYS ORBIT TIME CDS PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- 05-001 FOT See List Jan 05 30832 Generic Late Acquisition 05-002 MPS 73008 012/1251 NA BATT 3 Diff Voltage High 05-003 MPS 73100 018/1538 N/A PMON GRP 31 AND ACTION 23 OOL 05-004 MACS 73134 020/2122 N/A Pitch Wheel Anomaly