******************************************************************** UARS WEEKLY STATUS REPORT - 29 JUN 2001 ******************************************************************** *********** SOLSTICE *********** SOLSTICE began day only operations on day 178 (6/27) in support of the yaw maneuver. We were subsequently turned offcompletely on day 179 due to low power conditions during the yaw. We expect to return to normal operations on day 182. Otherwise, SOLSTICE continues to operate normally, taking solar data on all available orbital tracking periods and stellar calibration observations whenever possible. We continue to gather enough data to meet all the SOLSTICE science objectives during this period of reduced tape recorder operations. *********** SUSIM *********** Nothing received. *********** ACRIM *********** Nothing received. *********** PEM *********** ***** ALL PEM COMMUNICATION SHOULD NOW BE THROUGH THE PEM2K:: NODE ***** The PEM team reports that the PEM:: node computer has failed and has been taken off line. PEM:: appears to have hardware problems that take the system down every few hours. Automatic transfer NRT tests to PEM2K have succeed however the NRT files have to be verified against those captured by PEM to confirm the NRT process is correct. PEM/AXIS was activated in its half power mode on June 24. At the current time, AXIS is not generating energy deposition. SwRI is looking into this. Tests of AXIS production code on the rehost computer are continuing. At the present time, PEM energy deposition from its spectrometers is not being generated. Recent data configuration changes have affected PEM software causing multiple failures. These failures are being reviewed by the PEM team. In order to correct for new telemetry requirements, PEM will need to update processing code with a patch delivery. The delivery patch may include changes which would allow the PEM software to execute on a DEC Alpha machine. GSFC is helping PEM with some DEC Alpha particulars which have caused PEM level 3 code to fail on DEC Alpha machines (software below level 3 executes on the DEC Alpha). Updated HEPS calibration parameters have been finalized and are ready for delivery. Updated MEPS quality calibration files have been finalized and are ready for delivery. Level 3 software errors, discovered by Dr. Dean Pesnell, have been fixed; his suggestions have been incorporated with in the PEM production code. Both updated HEPS and MEPS calibration data, along with the Level 3 code changes, will influence the in-situ energy deposition predictions, so new versions of PEM energy deposition Level 3 files will be generated. *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 *********** On 27 June 2001 the MPG participated in the UARS Monthly Status Review Meeting. Normally, these meetings are held on the first Wednesday of each month. Since the first Wednesday of July is a holiday, this meeting was moved to the last week of June. Daily processing of instrument Daily Activity Plans continues with no problems. *********** CDHF *********** Following one week of parallel operations between the UARS CHDF legacy system and the Rehost system that began on June 18, the operational transition to production processing on the Rehost system occurred on June 25. The NRT data flow remains on the legacy system and will be moved to the Rehost system during the week of July 9. The NRT was not moved earlier due to the planned yaw maneuver on June 28 and other test activities and the holiday during the week of July 2. *********** FOT *********** REPORTING PERIOD This report covers 16 June 2001 (Orbit 53371, GMT Day 167) through 22 June 2001 (Orbit 53475, GMT Day 173). 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 WINDII 169/0403 53403 Power OFF (S/C Low Power) HALOE 172/1424 53454 Power OFF HALOE 172/1745 53456 Power ON SOLSTICE 172/1827 53457 Power ON ACRIM 172/1827 53457 Power ON SUSIM 172/1928 53457 Power ON SUSIM 172/2145 53459 Power ON HRDI 173/0225 53462 Power ON The beta angle ranged between the angles of 32.8 degrees to 21.7 degrees for this report period. The beta angle is now decreasing towards a minimum angle of 0 degrees on 28 June 2001 (DOY 179). 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 23.8 V end-of-night (EON) load bus voltage. Battery temperatures are stable with a temperature delta between Battery 2 and Battery 3 of 1.3 to 1.6 degrees C. Additional battery performance data for each battery on 15 June 2001 and 22 June 2001 are provided in Appendix D. The clock error ranged from Ð11.8 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 = 13 ¥ ALERTS = 00 The following real-time command sheets were executed for the listed operational element(s) during this report period (see Appendix A). ¥ FOT = 19 ¥ WINDII = 01 ¥ HALOE = 02 ¥ SOLSTICE = 01 ¥ ACRIM = 01 ¥ SUSIM = 02 ¥ HRDI = 01 UARS Anomaly Reports initiated during this report period are listed in Appendix E and summarized below. ¥ FOT = 02 One (1) Anomaly Reports remained OPEN at the end of this report period (see Appendix E). TRANSPONDER FREQUENCIES: · Transponder A: 00/316 - 2287.496493 · Transponder B: 01/119 - 2287.499116 GROUND SYSTEM OPERATION Two (2) operational support problems occurred this period. Anomaly Reports are included in Appendix E. The data loss calculations supplied by Data Capture Facility (DCF) from mission start through UTC Day 01/158 show the observatory data loss to be 301 hours, 02 minutes, 12.728 seconds. This shows zero loss since the last report period. This is a 0.39 percent data loss, which equals a 99.61 percent data capture for the mission. OTHER SIGNIFICANT EVENTS UARS SATELLITE OPERATIONS The FOT continues to fine-tune the TAM alignment by loading new alignment matrices. A new alignment is required for the reverse flight direction. This is a slow process and it will take many alignments to lock in on the most accurate solution. An instrument anomaly was experienced on 05 May 2001. The instrument involved was the ACRIM II instrument. All ACRIM telemetry for currents and voltages all dropped to zero values suddenly. The ACRIM team in coordination with the UARSFOT is conducting analysis and command tests to determine the cause of the anomaly. Analysis shows that the anomaly was caused due to failed circuitry in the ACRIM electronics box. The FOT is awaiting a future plan of action from the ACRIM team. MEETINGS The FOT attended a UARS SERB/TAC RS Meeting on Wednesday, June 20, 2001. FUTURE SIGNIFICANT EVENTS The next UARS Yaw slew is scheduled for 28 June 2001 (DOY 179). This maneuver will be a Reverse to Forward Flight maneuver (Southern Hemisphere viewing). Attachments: Appendix A, Real-time Commands 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 22 June 2001 ORBIT AOS NO. SUBSYS REASON ----- --- --- ------ ------ 53373 167/0440 01-393 NBTR NOOPS D-167 53381 167/1742 01-393 NBTR NOOPS D-167 53382 167/1824 01-395 NBTR NOOPS D-168 53389 168/0540 01-395 NBTR NOOPS D-168 53396 168/1742 01-396 NBTR NOOPS D-169 53403 169/0403 01-397 WINDII Power OFF (S/C Low Power) 53404 169/0539 01-396 NBTR NOOPS D-169 53405 169/0720 01-398 OBC Clk Adj fr 0.00 to 20.6 msec/day 53411 169/1743 01-396 NBTR NOOPS D-169 53412 169/1825 01-399 NBTR NOOPS D-170 53419 170/0540 01-399 NBTR NOOPS D170 53421 170/0908 01-400 OBC Clk Adj fr 20.6 to 0.00 msec/day 53426 170/1743 01-399 NBTR NOOPS D170 53433 171/0443 01-401 NBTR NOOPS D171 53442 171/1826 01-402 NBTR NOOPS D172 53449 172/0626 01-402 NBTR NOOPS D172 53454 172/1424 01-403 HALOE Power OFF 53456 172/1745 01-405 HALOE Power ON 53457 172/1827 01-406 SOLSTICE Power ON 53457 172/1827 01-407 ACRIM Power ON 53457 172/1827 01-404 NBTR NOOPS D173 53457 172/1928 01-408 SUSIM Power ON 53459 172/2145 01-409 SUSIM Power ON 53462 173/0225 01-410 HRDI Power ON 53463 173/0445 01-411 OBC Clk Adj fr 0.0 to -20.6 msec/day 53464 173/0627 01-404 NBTR NOOPS D173 53472 173/1746 01-412 NBTR NOOPS D174 ______________________________________________________________________________ APPENDIX B OUT-OF-LIMITS & ALERTS OCCURRENCES Week ending 22 June 2001 The following Out-Of-Limits occurrences were detected: MNEMONIC STATE DESCRIPTION ORBITS -------- ----- ----------- ------ WIQBVOLTAGE Y-LO WINDII Quiet Bus Voltage 53373-6 HRPSEQBIMON Y-HI PSE Quiet Bus Current Monitor 53373-6 WIQBVOLTAGE Y-LO WINDII Quiet Bus Voltage 53387-90 HRPSEQBIMON Y-HI PSE Quiet Bus Current Monitor 53388-90 CDUNRG28 Y-LO +28 UNREG Bus 53388-90 WIQBVOLTAGE Y-LO WINDII Quiet Bus Voltage 53402-3 HRPSEQBIMON Y-HI PSE Quiet Bus Current Monitor 53402-3 PWLBV Y-LO Load Bus Voltage 53402-3 PWBAT3V Y-LO Battery 3 Voltage 53402-3 CDUNRG28 Y-LO +28 UNREG Bus 53402-3 PWLBV Y-LO Load Bus Voltage 53402-3 PWBAT2V Y-LO Battery 2 Voltage 53454 PWBAT3V Y-LO Battery 3 Voltage 53454 The following ALERT occurrences were detected: MNEMONIC DESCRIPTION ORBITS -------- ----------- ------ -None this report period _______________________________________________________________________________ APPENDIX C CLOCK & SOLAR ARRAY RATE CORRECTIONS Week ending 22 June 2001 CLOCK DRIFT RATE ADJUSTMENTS ORBIT TIME CLOCK RATE CHANGE ----- ----- ----------------- 53405 169/0723 Clk Adj fr 0.00 to 20.6 msec/day 53421 170/0911 Clk Adj fr 20.6 to 0.00 msec/day 53463 173/0449 Clk Adj fr 0.0 to -20.6 msec/day _______________________________________________________________________________ APPENDIX D UARS BATTERY PERFORMANCE DATA Week ending 22 June 2001 15 June 2001 - GMT Day 166 Beta = 33.4 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 -3.05/-4.31 +0.0/+0.0 12.0 0.000 0.0 2 +11.2/-78.4 +6.44/+4.51 +28.4/-15.2 23.8 1.030 20.2 3 +16.8/-89.6 +5.15/+3.55 +28.0/-15.2 23.8 1.020 19.9 22 June 2001 - GMT Day 173 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 +728.0/+728.0 -3.05/-4.31 +0.0/+0.0 12.0 0.000 0.0 2 +11.2/-112.0 +5.79/+4.51 +28.8/-14.4 24.5 1.040 20.8 3 +22.4/-56.0 +4.83/+3.23 +28.4/-14.4 24.3 1.040 20.5 V/T LEVEL CHANGES ORB# TIME LVL FR-TO ---- ---- --------- -no changes V/T 5 _______________________________________________________________________________ APPENDIX E UARS ANOMALY REPORTS Week ending 08 June 2001 NEW ANOMALY REPORTS GENERATED AR NO. SUBSYS ORBIT TIME TTR PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- 01-032 FOT 53437 171/0947 14170 Generic Late Acquisition 01-038 FOT 53454 172/1424 N/A TMON 1, 2 TRIPPED ANOMALY CLOSURE INFORMATION RECEIVED AR NO. SUBSYS ORBIT TIME TTR PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- 01-033 FOT 53222 157/0220 N/A CDEL function not working 01-034 FOT 53225 157/0754 N/A Unable to dump ATC 01-037 FOT 53292 161/1820 N/A Unable to load ATC 01-038 FOT 53454 172/1424 N/A TMON 1, 2 TRIPPED 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 ------ ------ ----- ---- --- ----------------- 01-032 FOT see list June 01 14170 Generic Late Acquisitio SEVNTFW01/25