******************************************************************** UARS WEEKLY STATUS REPORT - 17 SEP 2004 ******************************************************************** ********************************************************** EMAIL from UARS Project Science Office (15 September 2004) ********************************************************** Dear UARS Investigators: Thirteen years ago yesterday, September 14th, the UARS was deployed from the Space Shuttle Discovery. We consider it our lucky "13th Anniversary of Deployment." The EOS Aura satellite was launched successfully in July of this year and we look forward to UARS providing at least a year of overlap of measurements to help in the validation and calibration of the new EOS Aura atmospheric-observing instruments. Five of the original ten UARS instruments collect data on a regular basis. These five instruments include HALOE, SUSIM, SOLSTICE, HRDI, and PEM. Although there have been some recent battery concerns, the skillful and professional UARS Flight Operations Team is in control of the situation and adjusts the battery charging as needed. We salute the many personnel who have made the UARS mission possible: Those who designed and built a spacecraft and instruments capable of lasting 13 years in space. Those who monitor the functionality of the instruments and provide daily activity plans. Those who monitor the spacecraft 24/7 and have overcome several very serious anomalies over the years. and Those who have harvested the 13 years of data providing breakthroughs in our scientific understanding of many processes related to the atmosphere. Thanks to all for your support over this many-year mission. Best regards, Charles Jackman & Anne Douglass UARS Project Science Office ******************************************************************** *********** SOLSTICE *********** This week, SOLSTICE continued to operate in good health gathering solar data on all available orbital tracking periods. On average, we received 55% of each day's data amounting to about 524 minutes of solar observing time per day. *********** SUSIM *********** As available telemetry time permitted, SUSIM successfully gathered daily mid (1.1 nm) resolution, MgII, occultation, solar pointing offset, and continuous monitoring scans. SUSIM operations were unusually and severely limited on several days during this past week because of the lack of telemetry time. *********** PEM *********** PEM wishes to congratulate everyone past and present for the 13 years of successful operations of the UARS! HEPSA data files are version 2. Currently, HEPSA data between 1991274 and 2004099 has been reprocessed and archived at the GSFC DAAC. MEPS data files are version 1. Processed MEPS data files at the DAAC archive are between 1991274 and 2004099. 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 recieved. *********** 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 04 September 2004 (Orbit 71044, GMT Day 248) through 10 September 2004 (Orbit 71149, GMT Day 254). 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 HALOE 250/1401 71083 POWER ON HALOE 251/0641 71094 POWER OFF HALOE 251/1539 71099 POWER ON HALOE 252/0420 71107 POWER OFF The beta angle ranged between the angles of 62.9 degrees to 58.1 degrees for this report period. The beta angle is now decreasing towards a minimum angle of 0 degrees on 25 September 2004 (DOY 269). 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 1.26 to 1.27 degrees C. Additional battery performance data for each battery on 03 September and 10 September 2004 are provided in Appendix D. The clock error ranged from 10.5 to -10.3 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 = 03 HALOE = 04 UARS Anomaly Reports initiated during this report period are listed in Appendix E and summarized below. FOT = 00 Zero (0) Anomaly Reports remained OPEN at the end of this report period (see Appendix E). GROUND SYSTEM OPERATION Zero (0) 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 On 10 August 2004, during the 223/0121 Z event, VT-6 was commanded due to the differential voltage being greater than 180 mV for three consecutive orbits. The differential voltage returned to nominal values after two orbits subsequent to the change. The spacecraft remained in VT-6 until approximately 245/1600, at which time it was commanded back to VT-5. All trending of the power subsystem during this time looks nominal and the FOT will continue to use VT-6 should the differential climb again. A new release of the CMS code to allow for SMA events was delivered to the backup CMS last week. This new release was built to fix the file transfer problem encountered in the previous build. The preliminary testing showed the file transfer issue to be resolved, but the build still requires all other process testing. The goal for completion is the end of September. MEETINGS The FOT attended the UARS Monthly Status Review on 07 September 2004 to review the significant events for the month of August. The FOT also attended the HRDI attitude meeting on 08 September2004. At this meeting it was decided that the CDHF functionality of generating the FDF attitude file, would be reexamined in an attempt to reprocess old data on the mini-CDHF. This is being done in the hope that it will give the HRDI team more accurate attitude knowledge to possibly correct their attitude discrepancy. FUTURE SIGNIFICANT EVENTS The next UARS Yaw slew is scheduled for 25 September 2004 (DOY 269). 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 10 September 2004 ORBIT AOS NO. SUBSYS REASON ----- --- --- ------ ------ 71049 248/0650 04-251 OBC/CLK CLK ADJ FR 0.0 TO 20.6 MSEC/DAY 71083 250/1401 04-252 HALOE POWER ON 71094 251/0641 04-253 HALOE POWER OFF (HATBAT HI) 71099 251/1539 04-254 HALOE POWER ON 71102 251/1918 04-255 OBC/CLK CLK ADJ FR 20.6 TO 0.0 MSEC/DAY 71107 252/0420 04-256 HALOE POWER OFF (TBAT) 71123 253/0551 04-257 OBC/CLK CLK ADJ FR 0.0 TO 20.6 MSEC/DAY APPENDIX B OUT-OF-LIMITS & ALERTS OCCURRENCES Week ending 10 September 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 10 September 2004 CLOCK DRIFT RATE ADJUSTMENTS ORBIT TIME CLOCK RATE CHANGE ----- ----- ----------------- 71049 248/0655 CLK ADJ FR 0.0 TO 20.6 MSEC/DAY 71102 251/1918 CLK ADJ FR 20.6 TO 0.0 MSEC/DAY 71123 253/0554 CLK ADJ FR 0.0 TO 20.6 MSEC/DAY APPENDIX D UARS BATTERY PERFORMANCE DATA Week ending 10 September 2004 03 September 2004 - GMT Day 247 Beta = 58.6 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 -700.0/-700.0 -3.05/-4.62 +00.0/+00.0 07.0 0.00 0.0 2 +22.4/-044.8 +3.87/+2.29 +20.8/-13.6 26.4 1.04 16.3 3 +11.2/-044.8 +3.23/+1.66 +20.8/-14.4 26.4 1.03 16.3 10 September 2004 - GMT Day 254 Beta = 58.1 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 -11.2/-067.2 +3.87/+2.60 +22.0/-14.4 26.4 1.03 15.9 3 -22.4/-112.0 +2.92/+1.66 +21.6/-14.4 26.2 1.02 15.9 V/T LEVEL CHANGES ORB# AOS TIME LVL FR-TO ----- -------- --------- -None this report period. APPENDIX E UARS ANOMALY REPORTS Week ending 10 September 2004 NEW ANOMALY REPORTS GENERATED AR NO. SUBSYS ORBIT TIME CDS PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- -None this report period. ANOMALY CLOSURE INFORMATION RECEIVED AR NO. SUBSYS ORBIT TIME CDS PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- 04-059 FOT 71015 246/0136 N/A OBC/CLK adj cmd problem 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 ------ ------ ----- ---- --- ----------------- -None this report period.