******************************************************************** UARS WEEKLY STATUS REPORT - 30 JUL 2004 ******************************************************************** *********** SOLSTICE *********** Nothing received. *********** SUSIM *********** SUSIM successfully gathered its daily mid (1.1 nm) resolution, MgII, occultation, solar pointing offset, and continuous monitoring scans for periods of UARS real-time telemetry or onboard tape recording. *********** 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 17 July 2004 (Orbit 70308, GMT Day 199) through 23 July 2004 (Orbit 70412, GMT Day 205). 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 SOLSTICE 203/1230 70375 DAY ONLY TO FULLTIME SUSIM 203/1552 70378 POWER ON PEM 204/1407 70391 OFF TO DAY ONLY A Forward-to-Reverse Yaw Around maneuver (number 131) was successfully executed in Orbit 70317 beginning 199/ 15:04:25Z and completing at 199/ 15:41:35Z on 17 July 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 57.89 minutes. Post maneuver analysis of data indicate that during the Yaw Around, the end-of-night load bus voltage was 26.08 volts and the average depths of discharge (DODs) on Batteries 2 and 3 were approximately 20.51 and 20.04 percent respectively. The next (reverse-to-forward) YAW is scheduled for 18 August 2004 (DOY 231). The beta angle ranged between the angles of 01.3 degrees to 19.2 degrees for this report period. The beta angle is now increasing towards a maximum angle of 39 degrees on 01 August 2004 (DOY 214). 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 0.63 to 0.96 degrees C. Additional battery performance data for each battery on 16 July and 23 July 2004 are provided in Appendix D. The clock error ranged from 10.8 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 = 03 SOLSTICE = 01 SUSIM = 01 PEM = 01 UARS Anomaly Reports initiated during this report period are listed in Appendix E and summarized below. FOT = 04 Three (3) Anomaly Report remained OPEN at the end of this report period (see Appendix E). GROUND SYSTEM OPERATION Four (4) 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 The FOT continued testing the new version of the Eclipse ground system software. There are several DR fixes incorporated in the build, so testing will take some time. The goal for the testing to be complete is the end of the July. If all testing is successful the new build will be released to operations. The new CMS code to allow for SMA events continued to undergo testing this week. Problems receiving products from FDF, transferring the schedule from UPS to CMS, and system drive issues hindered progress. While the system drive issues have been resolved, the other two issues are still under investigation. MEETINGS -None this report period. FUTURE SIGNIFICANT EVENTS The next UARS Yaw slew is scheduled for 18 August 2004 (DOY 231). 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 23 July 2004 ORBIT AOS NO. SUBSYS REASON ----- --- --- ------ ------ 70317 199/1449 04-210 MACS YAW MANEUVER COMMANDS 70326 200/0623 04-211 OBC/CLK CLK ADJ FR 0.0 TO -20.6 MSEC/DAY 70347 201/1457 04-210 MPS VT-6 TO VT-5 70348 201/1638 04-212 OBC/CLK CLK ADJ FR -20.6 TO 0.0 MSEC/DAY 70375 203/1230 04-213 SOLSTICE DAY ONLY TO FULLTIME 70378 203/1552 04-214 SUSIM POWER ON (PARTIAL) 70390 204/1227 04-214 SUSIM POWER ON (COMPLETE) 70391 204/1407 04-215 PEM OFF TO DAY ONLY APPENDIX B OUT-OF-LIMITS & ALERTS OCCURRENCES Week ending 23 July 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 23 July 2004 CLOCK DRIFT RATE ADJUSTMENTS ORBIT TIME CLOCK RATE CHANGE ----- ----- ----------------- 70326 200/0630 CLK ADJ FR 0.0 TO -20.6 MSEC/DAY 70348 201/1639 CLK ADJ FR -20.6 TO 0.0 MSEC/DAY APPENDIX D UARS BATTERY PERFORMANCE DATA Week ending 23 July 2004 16 July 2004 - GMT Day 198 Beta = 04.7 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 -3.68/-4.31 +00.0/+00.0 07.0 0.00 0.0 2 -05.6/-22.4 +4.51/+3.87 +16.8/-12.0 26.7 1.11 18.8 3 +16.8/-22.4 +3.55/+2.92 +16.0/-11.6 26.7 1.11 18.4 23 July 2004 - GMT Day 205 Beta = 04.7 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 -3.68/-4.94 +00.0/+00.0 07.0 0.00 0.0 2 -00.0/-44.8 +4.19/+3.23 +27.2/-12.8 26.2 1.01 18.5 3 +11.2/-72.8 +2.92/+2.29 +25.6/-12.8 26.2 1.00 18.1 V/T LEVEL CHANGES ORB# AOS TIME LVL FR-TO ----- -------- --------- 70347 200/1457 VT6 -> VT5 APPENDIX E UARS ANOMALY REPORTS Week ending 23 July 2004 NEW ANOMALY REPORTS GENERATED AR NO. SUBSYS ORBIT TIME CDS PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- 04-039 FOT 70335 200/2037 30832 Generic Late Acquisition 04-039 FOT 70335 202/0800 30832 Generic Late Acquisition 04-047 FOT 70367 202/2252 N/A WS-4 not responding properly 04-048 FOT 70395 204/1920 36444 Data Dropout ANOMALY CLOSURE INFORMATION RECEIVED AR NO. SUBSYS ORBIT TIME CDS PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- 04-043 FOT 70203 192/0155 30824 Data Dropout (18 sec) 04-044 SSPP 70234 194/0229 N/A SSPP File Xfer Error on CMS 04-045 FOT 70258 195/1750 36367 Data Dropout @ White Sands 04-046 FOT 70290 197/2031 36385 Data Dropout Bad Weather @ WS 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 ------ ------ ----- ---- --- ----------------- 04-039 FOT See List July 04 30832 Generic Late Acquisition 04-047 FOT 70367 202/2252 N/A WS-4 not responding properly 04-048 FOT 70395 204/1920 36444 Data Dropout