UARS Weekly Status Report

03 DECEMBER 1999




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                UARS WEEKLY STATUS REPORT - 03 DEC 1999

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SOLSTICE
***********

SOLSTICE continues to operate normally, collecting solar data on all 
available orbital tracking periods and stellar calibration observations, 
whenever possible.

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SUSIM
***********

In spite of continuing telemetry outages, the SUSIM was scheduled this
past week for a normal set of solar scans.  Although these were
apparently successful, only about 75% of the data were retrieved. 
Potentially, this could raised to 100% if the times of telemetry
availability are known at the time when SUSIM's plans are written.

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ACRIM
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Nothing received.

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PEM
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     The PEM/AXIS was operated from November 22 through November 28.  During
this time, AXIS computed energy deposition from electrons which were derived
from the measured X-ray spectrum.  All 16 of the AXIS pixels were active.

     The PEM spectrometers continue to be active under PMON control*.  While 
under PMON control, the PEM spectrometers computed energy deposition from 
electrons and protons measured in-situ by the particle spectrometers.


*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.

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HALOE 
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Nothing received.

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MLS
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Nothing received.

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HRDI
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Nothing received.

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WINDII
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Nothing received.

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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. The 
schedule of planned instrument operations for the next yaw 
cycle (8 December 1999 to 6 January 2000) was distributed.

The MPG has continued to assist the FOT with analysis of the 
current tape recorder anomaly (NBTR B) and its impact on 
science data collection.  

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CDHF
***********

The CDHF continues to notify all PI Software Representatives when Data Gaps
occur in the LEVEL0 data due to the UARS Spacecraft Anomaly.
The CDHF notified all PI Software Representatives regarding the re-ingest of
UARS DAY 2998 Version 3 for better quality and more data.  Appropriate
production reprocessing was done against the Version 3 data.
   
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.
        18 days CLA (7.0)   PROD (L1-L3)         (476R-418C-21F=37L)
        15 days GPI (4.05)  PROD (CLAES L3B)     (372R-332C-2F=38L)
        41 days WIN (5.11A) PROD (L1-L3)         (520R-60C-4F=456L)
     
UARS CDHF REHOST:
   -  Testing SUSIM V7.1 on the Rehost System.
   -  Preparing to test SOLSTICE V4.62 on the Rehost
      System.
   -  Rehost procedures continued to be developed and/or reviewed. 
   -  Migration for all data levels continued. 
                                            
CDHF pending software upgrades: none
                  
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FOT
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REPORTING PERIOD

This report covers 20 November, 1999 (Orbit 44765, GMT Day 324) through 26 
November 1999 (Orbit 44869, GMT Day 330).


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      326/0046     44795     On
             PEM        326/1214     44802     AXIS On
            HALOE       329/1714     44850     On
            WINDII      330/2312     44869     Off

The beta angle ranged between the angles of 74.9 degrees to 50.3 degrees for 
this report period.  The beta angle is now decreasing toward a minimum angle of 
-2.0 degrees on 08 December 1999 (DOY 342).

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 19 November 1999 and 26 November 1999 are provided in Appendix D.

The clock error ranged from -11.4 to 11.4 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  =   11

The following real-time command sheets were executed for the listed operational 
element(s) during this report period (see Appendix A).

%     FOT     =     07
%     HRDI    =     03
%     WINDII  =     02
%     PEM     =     01
%     HALOE   =     01

UARS Anomaly Reports initiated during this report period are listed in Appendix 
E and summarized below.

%     FOT     =     02

Three (3) Anomaly Reports remained OPEN at the end of this report period (see 
Appendix E).

TRANSPONDER FREQUENCIES:
%     Transponder A:  99/284  -  2287.496981
%     Transponder B:  99/265  -  2287.498700


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 99/329 show the observatory data loss to be 185 hours, 19 
minutes, 46.873 seconds (an increase of 34 hours 22 minutes 56.768 seconds 
since the last report period).  This is a 0.2587 percent data loss which equals 
a 99.7413 percent data capture for the mission.

The increase of 34 hours 22 minutes 56.768 seconds occurred over seven (7) 
days:

7 00 hours 03 minutes 16.192 seconds on Day 323 due to a S/C TR problem.
7 00 hours 01 minutes 45.312 seconds on Day 324 due to a S/C TR problem.
7 00 hours 02 minutes 37.312 seconds on Day 325 due to a S/C TR problem.
7 05 hours 50 minutes 16.000 seconds on Day 326 due to a S/C TR problem.
7 11 hours 25 minutes 45.824 seconds on Day 327 due to a S/C TR problem.
7 08 hours 37 minutes 29.120 seconds on Day 328 due to a S/C TR problem.
7 08 hours 22 minutes 47.008 seconds on Day 329 due to a S/C TR problem.


OTHER SIGNIFICANT EVENTS

UARS SATELLITE OPERATIONS

NBTR B anomalies continued again on Monday, Nov. 22, 1999.  By Tuesday morning 
all PASS 1 data was non recoverable.  NBTR B operation continued throughout the 
week with only PASS 2 data captured.  Real-time supports were increased to 
compensate for the lost PASS 1 data.  The current plan for NBTR B operations 
are the following:

* Resume maximum coverage with a combination of TDRSS SSA and MA supports.
* Continue NBTR B anomaly testing and analysis.
* Continue NBTR B operations in 4-Mux mode.
* Coordinate real-time supports with PASS 2 coverage.
* Determine if PASS 2 and real-time operations can fulfill mission objectives.  
  Currently only 56 to 62 minutes in a 96 minute orbit possible for real-time 
  operations.
* Review possibility of modification to UARS flight software and ground system 
  to accept three TDRSS inputs to provide maximum orbital coverage.
* Review science priorities with acquisition strategy to maximize science 
  return.  Initial science assessment by mid December.  Final science review in 
  early January.

The Flight Operations Team completed the ERASE command test on Tuesday, Nov. 
23, 1999.  A /RAW command was used to send the Serial Magnitude command that 
was identified to the FOT to turn ERASE on.  The FOT initiated this command in 
two forms, wind and erase as two separate commands and as a composite command.  
The ERASE function did not activate in either test scenario.  To ensure that 
the ERASE did not activate even though telemetry showed the contrary, PASS 2 
was recorded, dumped and evaluated.  The PASS 2 data evaluated from this test 
was determined to be non-recoverable.


YEAR 2000 OPERABILITY SUPPORT

All areas identified to or by the Flight Operations Team for Y2K testing have 
been completed.  There are no other areas identified at this time that have not 
been Y2K certified.


MEETINGS

No relevant meetings this week.


FUTURE SIGNIFICANT EVENTS

No specific date was agreed upon for UARS Safehold configuration discussions.  
Instead, the Supporting Engineers involved will be contacted every two weeks to 
determine if either the Flight Operations Team or Supporting Engineers have any 
new developments that should be discussed in a group.  It is expected that one 
more meeting will be held before Y2k as an update to UARS safehold expectations 
for the new century.

UARS has tested and prepared for the Year 2000 event.  Special considerations 
have been made in preparation for a non nominal 1999 to 2000 transition.

The next UARS Yaw slew is scheduled for December 8, 1999.  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 26 November 1999

ORBIT        AOS         NO.     SUBSYS     REASON
-----        ---        ---      ------     -------
44775     324/1610     99-388     HRDI     SAFEHOLD DUE TO HIGH BARREL TEMP
44788     325/1240     99-389     HRDI     SAFEHOLD DUE TO HIGH BARREL TEMP
44795     326/0046     99-390     WINDII   POWER ON
44800     326/0734     99-377     HRDI     SAFEHOLD DUE TO HIGH BARREL TEMP
44802     326/1214     99-391     OBC      CLK ADJ.  41.2 to 20.6 MSEC/DAY
44802     326/1214     99-392     PEM      AXIS ON
44809     326/2221     99-393     TMON     DISA TMON 37 RPT
44821     327/1713     99-394     NBTR     NBTR SPOOLING
44822     327/1858     99-395     NBTR     NBTR FFWD ERASE
44825     328/0048     99-396     OBC      TRANSMITTER NOOPS
44835     328/1627     99-397     OBC      CLK ADJ.  20.6 to 41.2 MSEC/DAY
44850     329/1714     99-398     HALOE    POWER ON
44858     330/0557     99-399     OBC      CLK ADJ.  41.2 to 20.6 MSEC/DAY
44869     330/2312     99-400     WINDII   POWER  OFF

__________________________________________________________________________

                       APPENDIX B
             OUT-OF-LIMITS & ALERTS OCCURRENCES
               Week ending 26 November 1999


The following Out-Of-Limits occurrences were detected:

MNEMONIC       STATE           DESCRIPTION               ORBITS
---------      -----          ------------               ------
HRPTSBARTMP     R-LO     HRDI TELESCOPE BARREL TEMP     44768-75
HRPTSBARTMP     Y-LO     HRDI TELESCOPE BARREL TEMP     44776-7
HRPTSBARTMP     Y-LO     HRDI TELESCOPE BARREL TEMP     44783-86,89
HRPTSBARTMP     R-LO     HRDI TELESCOPE BARREL TEMP     44787-89
QTZEPSIF1       Y-LO     ZEPS I/F PLATE AFT             44789-91
HRPTSBARTMP     Y-LO     HRDI TELESCOPE BARREL TEMP     44797,801
HRPTSBARTMP     R-LO     HRDI TELESCOPE BARREL TEMP     44798-800
HRPTSBARTMP     Y-LO     HRDI TELESCOPE BARREL TEMP     44815-24
HRPTSBARTMP     R-LO     HRDI TELESCOPE BARREL TEMP     44821
HRPTSBARTMP     Y-LO     HRDI TELESCOPE BARREL TEMP     44825-35
HRPTSPBIMON     Y-HI     HRDI Telescope Barrel          44847




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 26 November 1999

                 CLOCK DRIFT RATE ADJUSTMENTS

ORBIT               TIME                CLOCK RATE CHANGE
-----               ----                -----------------
44802     326/12:20 (22 Nov 99)     from 41.2 to 20.6 msec/day
44835     328/16:30 (24 Nov 99)     from 20.6 to 41.2 msec/day
44858     330/06:00 (26 Nov 99)     from 41.2 to 20.6 msec/day

________________________________________________________________________

                        APPENDIX D
               UARS BATTERY PERFORMANCE DATA
               Week ending 26 November 1999

     19 Nov 1999 - GMT Day 323 Beta = 74.9 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    -67.2/-89.6   -2.42/-3.36   +0.0/+0.0    16.3     0.000      0.0
2    +22.4/+0.0    +3.23/+1.66  +16.8/-14.8   27.5     1.037     13.4
3    +22.4/-22.4   +2.29/+1.34  +16.0/-14.4   27.4     1.035     12.9

     26 Nov 1999 - GMT Day 330 Beta = 50.3 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    -56.0/-78.4    -3.68/-4.94   +0.0/+0.0     16.2    0.000      0.0
2    +84.0/+0.0     +5.47/+4.19  +28.4/-16.0    25.3    1.030     19.5
3    +22.4/-22.4    +4.51/+2.92  +27.2/-15.2    25.1    1.027     19.1

       V/T LEVEL CHANGES
ORB#      TIME     LVL FR-TO
-----     ---      ----------
     no changes     V/T 5

                        APPENDIX E
                    UARS ANOMALY REPORTS
                Week ending 26 November 1999

                 NEW ANOMALY REPORTS GENERATED
AR NO.   SUBSYS    ORBIT      TIME      TTR     PROBLEM/DATA LOSS
------   ------    -----      ----      ---     -----------------
99-085    FOT     44810     327/0008   21603    512 kb playbacks errors
99-086    FOT     44823     327/2109   21606    TPF - No I channel
99-081    FOT     44843     329/0509   14170    Generic Late Acquisition

           ANOMALY CLOSURE INFORMATION RECEIVED
AR NO.   SUBSYS    ORBIT     TIME       TTR     PROBLEM/DATA LOSS
------   ------    -----     ----       ---     -----------------
99-085    FOT     44810     327/0008    21603    512 kb playbacks errors
99-086    FOT     44823     327/2109    21606    TPF - No I channel

        ANOMALY INVESTIGATION REPORTS GENERATED
AR NO.     SUBSYS     ORBIT     TIME     TTR     PROBLEM/DATA LOSS
------     ------     -----     ----     ---     -----------------
                 No new reports generated

                 OPEN ANOMALY REPORTS
AR NO.    SUBSYS   ORBIT       TIME      TTR     PROBLEM/DATA LOSS
------    ------   -----       ----      ---     -----------------
99-064     FOT     44135     10/8-9/99   N/A     HRDI Cal Lamp Errors
99-071     FOT     44398      299/1212   21512   TPF Not Receiving 512 PB
99-081     FOT                November   14170   Generic Late Acquisition

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