******************************************************************** UARS WEEKLY STATUS REPORT - 10 Dec 2004 ******************************************************************** *********** SOLSTICE *********** Nothing received. *********** SUSIM *********** SUSIM resumed operations on Monday, Dec. 6. Since then, the experiment 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. A solar minimum spectrum derived from the SUSIM UV spectral irradiance data is available from the SUSIM internet site. Details may be found from: http://wwwsolar.nrl.navy.mil/susim_uars_news.html *********** PEM *********** Nothing received. *********** 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 27 November 2004 (Orbit 72308, GMT Day 332) through 03 December 2004 (Orbit 72413, GMT Day 338). 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 HALOE 333/2321 72338 POWER OFF PEM 335/2317 72368 POWER OFF SUSIM 336/2234 72382 POWER OFF SOLSTICE 336/2315 72383 FULL TIME TO DAY ONLY A Forward-to-Reverse Yaw Around maneuver (number 135) was successfully executed in Orbit 72393 beginning 337/ 15:19:59Z and completing at 337/ 15:57:09Z on 02 December 2004. All instruments were in their off or standby mode (except for SOLSTICE in day-only). Due to the SA position at 269 degrees, the effective night length of the spacecraft after the maneuver was approximately 57.34 minutes. Post maneuver analysis of data indicate that during the Yaw Around, the end-of-night load bus voltage was 25.92 volts and the average depths of discharge (DODs) on Batteries 2 and 3 were approximately 20.16 and 20.04 percent respectively. The next (reverse-to-forward) YAW is scheduled for 12 January 2005 (DOY 012). The beta angle ranged between the angles of 18.2 degrees to 03.7 degrees for this report period. The beta angle is now increasing towards a maximum angle of 80 degrees on 23 December 2004 (DOY 358). 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 0.64 to 0.95 degrees C. Additional battery performance data for each battery on 26 November and 03 December 2004 are provided in Appendix D. The clock error ranged from 10.9 to -09.9 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 = 04 HALOE = 01 PEM = 02 SUSIM = 01 SOLSTICE = 01 UARS Anomaly Reports initiated during this report period are listed in Appendix E and summarized below. FOT = 01 One (1) Anomaly Report remained OPEN at the end of this report period (see Appendix E). GROUND SYSTEM OPERATION One (1) operational support problem 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 called a meeting with FORMATS' software development to discuss the file transfer issues from the UARS UPS to the UARS CMS via FORMATS. Software development was informed of problems being seen in the file. They will now look into their configuration tables and scripts, to see if the cause can be isolated and/or fixed. The FOT will call another meeting next week to review their progress. MEETINGS The FOT called a meeting with FORMATS and CMS software development on 30 November 2004 to discuss the SMA problems. FUTURE SIGNIFICANT EVENTS The next UARS Yaw slew is scheduled for 12 January 2005 (DOY 012). This maneuver will be a Reverse to Forward Flight maneuver (Southern 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 03 December 2004 ORBIT AOS NO. SUBSYS REASON ----- --- --- ------ ------ 72311 332/0432 04-328 OBC/CLK CLK ADJ FR -20.6 TO 0.0 MSEC/DAY 72338 333/2321 04-329 HALOE POWER OFF 72368 335/2317 04-330 PEM POWER OFF 72379 336/1755 04-331 OBC/CLK CLK ADJ FR 0.0 TO -20.6 MSEC/DAY 72382 336/2234 04-332 SUSIM POWER OFF 72383 336/2315 04-333 SOLSTICE FULL TIME TO DAY ONLY 72392 337/1434 04-334 MACS YAW MANEUVER 72393 337/1515 04-335 PEM YAW COMMANDS 72393 337/1515 04-334 MACS YAW MANEUVER 72393 337/1628 04-335 PEM YAW COMMANDS 72393 337/1628 04-334 MACS YAW MANUEVER 72399 338/0142 04-336 OBC/CLK CLK ADJ FR -20.6 TO 0.0 MSEC/DAY APPENDIX B OUT-OF-LIMITS & ALERTS OCCURRENCES Week ending 03 December 2004 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 03 December 2004 CLOCK DRIFT RATE ADJUSTMENTS ORBIT TIME CLOCK RATE CHANGE ----- ----- ----------------- 72311 332/0442 CLK ADJ FR -20.6 TO 0.0 MSEC/DAY 72379 336/1807 CLK ADJ FR 0.0 TO -20.6 MSEC/DAY 72399 338/0144 CLK ADJ FR -20.6 TO 0.0 MSEC/DAY APPENDIX D UARS BATTERY PERFORMANCE DATA Week ending 03 December 2004 26 November 2004 - GMT Day 331 Beta = 21.7 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 -2.74/-3.99 +00.0/+00.0 07.0 0.00 0.0 2 22.4/ -50.4 +6.43/+5.14 +28.8/-14.4 26.2 1.04 19.3 3 11.2/ -67.2 +5.14/+3.87 +28.0/-14.8 26.1 1.04 19.0 03 December 2004 - GMT Day 338 Beta = 03.7 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/-4.31 +00.0/+00.0 07.0 0.00 0.0 2 22.4/ -89.6 +5.46/+4.82 +27.2/-12.8 25.9 1.04 19.1 3 -11.2/-212.8 +4.50/+3.55 +26.8/-12.8 25.8 1.03 18.6 V/T LEVEL CHANGES ORB# AOS TIME LVL FR-TO ----- -------- --------- -None this report period APPENDIX E UARS ANOMALY REPORTS Week ending 03 December 2004 NEW ANOMALY REPORTS GENERATED AR NO. SUBSYS ORBIT TIME CDS PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- 04-086 FOT 72338 334/0024 30832 Generic Late Acquisition ANOMALY CLOSURE INFORMATION RECEIVED AR NO. SUBSYS ORBIT TIME CDS PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- 04-089 FOT 72289 330/1816 37679 TDRSS-E Data Dropout 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 ------ ------ ----- ---- --- ----------------- 04-086 FOT See List Nov 04 30832 Generic Late Acquisition