******************************************************************** UARS WEEKLY STATUS REPORT - 08 OCT 1999 ******************************************************************** *********** SOLSTICE *********** SOLSTICE continues to operate normally, collecting solar data on all available orbital tracking periods and stellar calibration observations, whenever possible. *********** SUSIM *********** Nothing received. *********** ACRIM *********** Nothing received. *********** PEM *********** Nothing receieved. *********** HALOE *********** Nothing received. *********** MLS *********** Nothing received. *********** HRDI *********** Nothing received. *********** WINDII *********** Nothing received. *********** MPG *********** Routine processing of instrument Daily Activity Plans continues with no problems. The MPG continues to assist the Project Scientist with the scheduling of instrument operations. *********** CDHF *********** The CDHF processed current day data through level 3 for all active instruments. Additionally, CDHF personnel reprocessed: (R)= Requested (C) = Complete, (F)= Failed (L) = Days remaining to reprocess. 13 days CLA (7.0) PROD (L1-L3) (473R-299C-16F=158L) 0 days GPI (4.05) PROD (CLAES L3B) (191R-164C-2F=25L) 21 days SUSIM (7.1) PROD (L1-L2) (56R-21C=35L) The CDHF plans on testing HALOE V4.82 formal delivery software, and then the WINDII delivery on the current CDHF. Current day data created and cataloged in July 1999 has been loaded into the DAAC Transfer Tables for HALOE, PEM, NMC, and UKMO. UARS CDHF REHOST: The CDHF continues to integrate the "UARS" environment on CDHFA/B. We are installing PI software - HALOE 4.82 new delivery - for testing. FDF was contacted to establish a process to test dataflows to the rehosted CDHF. CDHF pending software upgrades: none *********** FOT *********** REPORTING PERIOD This report covers 25 September, 1999 (Orbit 43927, GMT Day 268) through 1 October 1999 (Orbit 44030, GMT Day 274). SPACECRAFT OPERATION The observatory is now in Foward 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 270/2122 43969 On The beta angle ranged between the angles of 1.2 degrees to 25.7 degrees for this report period. The beta angle is now increasing toward a maximum angle of 50 degrees on 12 October 1999 (DOY 285). 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 1.0 to 1.3 degrees C. Additional battery performance data for each battery on 24 September 1999 and 01 October 1999 are provided in Appendix D. The clock error ranged from -9.9 to -2.1 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. % ALERTS = 00 % OUT-OF-LIMITS = 05 The following real-time command sheets were executed for the listed operational element(s) during this report period (see Appendix A). % HALOE = 02 UARS Anomaly Reports initiated during this report period are listed in Appendix E and summarized below. % FOT = 02 Zero (0) Anomaly Reports remained OPEN at the end of this report period (see Appendix E). TRANSPONDER FREQUENCIES: % Transponder A: 99/242 - 2287.496953 % Transponder B: 99/243 - 2287.499030 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 99/273 show the observatory data loss to be 24 hours, 55 minutes, 36.724 seconds (an increase of 10.656 seconds since the last report period). This is a 0.0354 percent data loss which equals a 99.9646 percent data capture for the mission. The increase of 10.656 seconds occurred over one (2) days: 7 2.080 seconds on Day 268 due to an Data hit. 7 8.576 seconds on Day 273 due to an Data hits, no overlap. OTHER SIGNIFICANT EVENTS UARS SATELLITE OPERATIONS Began preparations for the Leonid shower in November. More information about the shower and the impact to UARS orbit is being requested from FDF. It is not expected to change much if at all. YEAR 2000 OPERABILITY SUPPORT We received all of the planning aids needed for all the time periods to be tested for Y2K. The CMS processing will be completed on Monday and testing will be done on Tuesday and Thursday of next week. Hopefully, in those two days we can complete everything that we need to verify mission success in the next millennium. MEETINGS The FOT attended a meeting at Goddard Corporate Park regarding the UARS Y2k status. The primary focus was to evaluate what the obsticles were to complete Y2k certification and put the process back on schedule. All in all the meeting was successful and testing will continue with the next product delivery from FDF. FUTURE SIGNIFICANT EVENTS A meeting to discuss the UARS Safehold configuration and concerns for the MPS and its batteries is planned for Wednesday, October 6. This meeting will be a closed meeting with only the FOT and specialized engineering support attending. PEM requested to have the timing in their turn on sequence tightened up in yet another area. This is expected to be accomplished within the next few weeks. The FOT plans on working with FDF to devise a plan to verify the integrity of the UAV files in an effort to prevent discrepancies between the FDF 3-day High Gain Gimbal Angles file (HGA), and the 4-week User Antenna View files (UAV). A problem occured where TDRS view periods were incorrect following a UARS yaw maneuver. PERSONNEL CHANGES None. 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 1 October 1999 ORBIT AOS NO. SUBSYS REASON ----- --- --- ------ ------- 43969 270/2122 99-328 HALOE Power ON 43972 271/0222 99-329 HALOE Power ON, COMPLETED ________________________________________________________________ APPENDIX B OUT-OF-LIMITS & ALERTS OCCURRENCES Week ending 1 October 1999 The following Out-Of-Limits occurrences were detected: MNEMONIC STATE DESCRIPTION ORBITS --------- ----- ------------ ------ HRPTSPBIMON R-LO HRDI PULSE BUS MONITOR 43969 PEMBIAS00E R-HI PEM BIAS 43976 HRPTSPBIMON Y-HI HRDI PULSE BUS MONITOR 44005,6,8,14 HRPTSQBIMON Y-HI HRDI QUIET BUS MONITOR 44014 HRPTSPBIMON Y-HI HRDI PULSE BUS MONITOR 44018,20,21-3 The following ALERT occurrences were detected: MNEMONIC DESCRIPTION ORBITS --------- ------------ ------ No Alerts to report this report period. _______________________________________________________________________________ APPENDIX C CLOCK & SOLAR ARRAY RATE CORRECTIONS Week ending 1 October 1999 CLOCK DRIFT RATE ADJUSTMENTS ORBIT TIME CLOCK RATE CHANGE ----- ---- ----------------- None this report period APPENDIX D UARS BATTERY PERFORMANCE DATA Week ending 1 October 1999 24 Sept 1999 - GMT Day 267 Beta = 1.2 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 -112.0/-134.4 -3.05/-4.62 +0.0/+0.0 16.5 0.000 0.0 2 +33.6/-22.4 +5.47/+4.51 +29.6/-14.4 24.3 1.014 21.6 3 +33.6/-33.6 +4.51/+3.23 +28.8/-15.2 24.3 1.016 21.1 DIFF V (mV) TEMP (C) CURR (amp) EON V AVE C/D AVE BAT MAX/MIN MAX/MIN MAX/MIN MIN RATIO DOD(%) --- ---------- -------- ---------- ----- ------- ------ 1 -112.0/-134.4 -2.73/-3.99 +0.0/+0.0 16.5 0.000 0.0 2 +16.8/-67.2 +6.44/+5.15 +30.4/-15.2 24.5 1.023 22.3 3 +22.4/-56.0 +5.47/+3.87 +30.0/-16.0 24.3 1.024 22.1 V/T LEVEL CHANGES ORB# TIME LVL FR-TO ----- ---- --------- no changes V/T 5 APPENDIX E UARS ANOMALY REPORTS Week ending 1 October 1999 NEW ANOMALY REPORTS GENERATED AR NO. SUBSYS ORBIT TIME TTR PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- 99-061 FOT 43970 270/2216 21402 NEGATIVE ACQ. 99-058 FOT 43998 272/1917 14170 GENERIC LATE ACQ. ANOMALY CLOSURE INFORMATION RECEIVED AR NO. SUBSYS ORBIT TIME TTR PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- 99-058 FOT see list Sept 99 14170 Generic Late Acq. 99-059 FOT 43827 261/0856 N/A TAC Crashed 99-060 FOT 43833 261/1906 N/A TAC Crashed 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 ------ ------ ----- ---- --- ----------------- None this report period SEVNTFW99/40