******************************************************************** UARS WEEKLY STATUS REPORT - 12 Apr 2002 ******************************************************************** *********** SOLSTICE *********** SOLSTICE entered day only operations on April 3rd due to low power conditions. We continue to perform default solar observations during this time. *********** SUSIM *********** SUSIM performed its daily mid-resolution and MgII solar scans during periods of predicted UARS telemetry. *********** ACRIM *********** Nothing received. *********** PEM *********** PEM continues to receive NMC data files from NOAA. No problems have been encountered. PEM support of the UARS Traceability Mission for the TIMED mission has been organized with the GVUI team. Predicted TIMED-UARS conjunctions from the high geographic latitudes were compared with the expected magnetic position and the PEM climatology. Positional and anticipated precipitation flux information showed that expected electron precipitation as a function of magnetic activity had the highest probably of a successful conjunction on April 19. Continued monitoring has shown changes in conjunction times. For conjunctions within 300 km, there are now 5 times shown: Contact # Date Day Time Geo Lat ILAT MLT Hemisphere (deg) (deg) (hr) 1 April 18 108 21:29 56.47 54.53 21.37 North 2 April 18 108 22:18 -56.91 65.92 10.58 South 3 April 18 108 23:06 56.93 57.59 22.07 North 4 April 23 113 15:44 -56.97 47.79 9.10 South 5 April 23 113 16:32 56.96 53.25 20.12 North Contacts are progressing to earlier times. Of coarse, what is important is when PEM passes through the aurora at the same time GUVI is imaging, and this does not mean that UARS and TIMED are in conjunction. *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 continues to serve as the point-of-contact for UARS instrument operations to support re-engineering of the UARS Mission Operations Concept to develop capabilities for the Science Traceability Mission. Daily processing of instrument Daily Activity Plans continues with no problems. *********** CDHF *********** Nothing received. *********** FOT *********** REPORTING PERIOD This report covers 30 March 2002 (Orbit 57679, GMT Day 089) through 05 April 2002 (Orbit 57784, GMT Day 095). 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 088/1039 57670 Power OFF HALOE 088/1334 57672 Power ON HALOE 089/1918 57691 Power OFF (TBAT TEMP) HALOE 089/2234 57693 Power ON ACRIM 093/0312 57741 Power OFF PEM AXIS 093/0312 57741 Power OFF The beta angle ranged between the angles of 52.42 degrees to 34.23 degrees for this report period. The beta angle is now decreasing towards a minimum angle of 0 degrees on 13 April 2002 (DOY 103). 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 24.96 V end-of-night (EON) load bus voltage. Battery temperatures are stable with a temperature delta between Battery 2 and Battery 3 of 1.31 to 1.63 degrees C. Additional battery performance data for each battery on 30 March 2002 and 05 April 2002 are provided in Appendix D. The clock error ranged from -15.9 to 11.1 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 = 01 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 WINDII = 01 ACRIM = 01 PEM AXIS = 01 SOLSTICE = 01 UARS Anomaly Reports initiated during this report period are listed in Appendix E and summarized below. FOT = 3 Three (3) Anomaly Reports remained OPEN at the end of this report period (see Appendix E). TRANSPONDER FREQUENCIES: Transponder A: 01/333 - 2287.496855 Transponder B: 02/043 - 2287.498879 GROUND SYSTEM OPERATION Three (3) 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 At the Eclipse Delta ORR on 04 April 2002, the Eclipse Ground System was officially approved as the flight operations ground system for UARS. This was necessary to meet the anticipated loss of MSOCC personnel on 05 April 2002; thereby, reducing the cost for the extended mission. Eclipse has been very stable and performing well; in addition, the flight operators are adapting at an overwhelming rate. There are only a few open issues that are being investigated; these as well as a few other minor fixes are currently in progress. Another database delivery will probably be scheduled in a few weeks, allowing for other discrepancies to be found and then incorporated into the planned changes. Efforts are currently being directed to the readiness of Eclipse for the upcoming yaw maneuver on 13 April 2002. MEETINGS The FOT attended a UARS Eclipse Delta ORR on Thursday, April 04, 2002. FUTURE SIGNIFICANT EVENTS The next UARS Yaw slew is scheduled for 13 April 2002 (DOY 103). 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 05 April 2002 ORBIT AOS NO. SUBSYS REASON ----- --- --- ------ ------ 57670 088/1039 02-106 HALOE Power OFF 57672 088/1334 02-107 HALOE Power ON 57682 089/0536 02-108 OBC/CLK Clk Adj 20.6 to 0.00 msec/day 57691 089/1918 02-109 HALOE Power OFF (TBAT TEMP) 57693 089/2234 02-110 HALOE Power ON 57710 091/0135 02-111 WINDII WIERRFIX FOR E03 ERROR CODE 57723 091/2232 02-112 OBC Clk Adj fr 0.00 to 20.6 msec/day 57741 093/0312 02/113 ACRIM Power OFF 57741 093/0312 02-114 PEM AXIS Power OFF 57741 093/0351 02-115 SOLSTICE to DAY ONLY Ops 57751 093/1829 02-116 OBC Clk Adj fr 20.6 to 0.00 msec/day APPENDIX B OUT-OF-LIMITS & ALERTS OCCURRENCES Week ending 05 April 2002 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 -------- ----------- ------ WIERRCODE WINDII Software Error Code 57710 ______________________________________________________________________ APPENDIX C CLOCK & SOLAR ARRAY RATE CORRECTIONS Week ending 05 April 2002 CLOCK DRIFT RATE ADJUSTMENTS ORBIT TIME CLOCK RATE CHANGE ----- ----- ----------------- 57682 089/0536 Clk Adj 20.6 to 0.00 msec/day 57723 091/2232 Clk Adj fr 0.00 to 20.6 msec/day 57751 093/1829 Clk Adj fr 20.6 to 0.00 msec/day APPENDIX D UARS BATTERY PERFORMANCE DATA Week ending 05 April 2002 30 March 2002 - GMT Day 089 Beta = 52.42 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 0.00/-16.8 -3.77/-4.38 +0.0/ -0.0 10.56 0.000 0.00 2 +11.2/-44.8 +5.14/+3.82 +25.2/-14.4 24.96 1.020 20.04 3 +16.8/-56.0 +3.82/+2.85 +24.0/-14.4 24.96 1.020 19.69 05 April 2002 - GMT Day 095 Beta = 34.23 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 -3.16/-4.38 +0.0/ -0.0 9.60 0.000 0.00 2 +11.2/-16.8 +4.48/+3.82 +26.8/-13.2 26.40 1.040 18.99 3 +11.2/-22.4 +3.82/+2.85 +25.6/-12.8 26.40 1.030 18.52 V/T LEVEL CHANGES ORB# TIME LVL FR-TO ----- ---- --------- -no changes V/T 5 APPENDIX E UARS ANOMALY REPORTS Week ending 05 April 2002 NEW ANOMALY REPORTS GENERATED AR NO. SUBSYS ORBIT TIME TTR PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- 02-014 FOT 57704 090/1653 14170 Generic Late Acquisition 02-023 FOT 57767 094/2027 24285 Early LOS on OMNI Pass 02-024 FOT 57783 095/2209 24285 SOLSTICE INOPS in Day ANOMALY CLOSURE INFORMATION RECEIVED AR NO. SUBSYS ORBIT TIME TTR PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- 02-011 FOT 57466 074/2033 N/A AP-7 Disc Drive Failure 02-013 FOT 57467 074/2116 N/A AP-1 Hang-up 02-016 FOT 57523 078/1413 N/A AP-1 Halt/Gateway Fail 02-017 FOT 57553 080/1522 N/A Multiple TAC Problems 02-018 FOT 57556 080/1930 N/A AP-1 Crashed 02-019 FOT 57579 082/0822 N/A AP Reboot 02-020 FOT 57591 083/0325 N/A AP 1 Crashed 02-021 FOT 57604 084/0022 N/A AP 1 Crashed 02-014 FOT See List Mar 02 N/A Generic Late Acquisition 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 ------ ------ ----- ---- --- ----------------- 02-004 SOLSTICE 56883 036/0050 N/A Solstice in Wrong Mode 02-023 FOT 57767 094/2027 24285 Early LOS on OMNI Pass 02-024 FOT 57783 095/2209 24285 SOLSTICE INOPS in Day