UARS Weekly Status Report

21 MAY 1999




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                UARS WEEKLY STATUS REPORT - 21 MAY 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.

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

SUSIM gathered its normal solar, offset, and occultation data without
apparent problems.

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PEM
***********

     PEM/AXIS was active from May 14 through May 18.  During this time,
PEM/AXIS generated deposition profiles from electron precipitation which
were inverted from measured X-rays.

     PEM, active under PMON control, was terminated on May 18 due to a
large energy drain on the UARS spacecraft.  While under PMON control, the 
PEM instrument computed energy deposition from its particle spectrometers.

     The FOT and the PEM team are completing close-out documentation on 
the HEPS Energy Processor trouble; however progress has been hampered 
with the departure of Peter Thomas.

***********
HALOE 
***********

HALOE has been successfully operating. Presently, HALOE is off, but is
scheduled to be powered on beginning of day May 29, 1999.

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MLS
***********

MLS was reactivated successfully on May 11 and operated until May 19 13:27 UTC
when the FOT needed to turn MLS off due to power constraints. MLS was reactived
on May 20 and is scheduled to operate through May 28. 

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HRDI
***********

Nothing received.

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WINDII
***********

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. 

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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.
         2 days CLA (7.0)  PROD (L1-L3)         (22R-12C-4F=6L)
         2 days HAL (4.81) PROD (L1-L3)         (2R-2C=0L)
         2 day  HRD (4.4)  PROD (L1-L3)(TEST)   (2R-2C=0L)
        50 days PEM (3.32) PROD (OA-L2)         (753R-718C-1F=34L)
        55 days WIN (5.11) PROD (LOG)           (1540R-1540C=0L)
        62 days WIN (5.11) PROD (L1-L3)         (1540R-512-4F=1024L)

March 1999 current day DAAC data will be loaded in May 1999.
                    
CDHF pending software upgrades:  DEC AXP Fortran 6.5, DEC AXP OPEN
VMS 6.2, OpenIngres. 
                  
***********
FOT
***********

REPORTING PERIOD


This report covers 08 May 1999 (Orbit 41830, GMT Day 128) through 14 May 
1999 (GMT Day 134).


SPACECRAFT OPERATION

The observatory is now in Forward Flight (Southern Hemisphere viewing) and 
is performing nominally under two-battery operations.  The instrument 
operational changes were:

                INSTRUMENT OPERATIONAL CHANGES

     Instrument     Time       Orbit     Comment
       ACRIM      130/2230     41873     Off
        MLS       131/0006     41874     On
      SOLSTICE    131/0015     41874     Day Only
        HRDI      131/0336     41876     Day Only
       HALOE      133/2246     41918     Off
      SOLSTICE    134/0025     41919     Full Time
       ACRIM      134/0059     41919     On
       WINDII     134/0059     41919     On
        PEM       134/1126     41926     AXIS On

The beta angle ranged between the angles of 26.0 degrees to 55.9 degrees 
for this report period.  The beta angle is now increasing toward a maximum 
angle of 77 degrees on 21 May 1999 (DOY 141).

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 0.7 to 1.3 degrees C.  Additional battery performance data 
for each battery on May 07 1999 and May 14 1999 are provided in Appendix D.

The clock error ranged from 11.1 to -11.2 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  =   02

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

%     FOT     03
%     ACRIM   02
%     PEM     02
%     MLS     01
%     HRDI    01
%     HALOE   01
%     WINDII  01

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

%     FOT     01
%     HRDI    01

One (1) Anomaly Report remained OPEN at the end of this report period (see 
Appendix E).

TRANSPONDER FREQUENCIES:
          Transponder A:  99/117  -  2287.496987
          Transponder B:  99/118  -  2287.498739


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 99/119 show the observatory data loss to be 
24 hours, 12 minutes, 39.348 seconds (an increase of 2.240 seconds since 
the last report period).  This is a 0.0361 percent data loss which equals a 
99.9639 percent data capture for the mission.

The increase of 2.240 seconds occurred over five (3) days:

7 1.056 seconds on Day 127 due to a data hit,
7 0.672 seconds on Day 132 due to a data hit,
7 0.512 seconds on Day 133 due to a data hit.


OTHER SIGNIFICANT EVENTS

UARS SATELLITE OPERATIONS

FOT personnel are supporting the IMOC (SCS-21) development effort.  The 
current work is a continuation of the SCS-21 UARS implementation effort 
done last year which culminated in a level 1 demonstration.

The FOT continues to investigate the feasibility of a new PMON action to 
change battery V/T curves based on loading to mitigate battery risks in sun 
pointing safehold.


YEAR 2000 OPERABILITY SUPPORT

The end-to-end testing that was scheduled to start this week has been 
delayed until next week to allow additional time for FDF to create special 
Y2K planning aids.


UARS PROPULSION MODULE B/D THRUSTER LINE FILL - No change


MEETINGS

FOT attended the weekly IMOC meetings on 12 May 1999.


FUTURE SIGNIFICANT EVENTS

The next UARS Yaw Around Maneuver (forward-to-reverse) is scheduled for 11 
June 1999 (DOY 162).


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 14 May 1999

ORBIT        AOS         NO.     SUBSYS         REASON
-----        ---        ---     ------         -------  
41845     129/0139     99-159    OBC      Clk Adj fr 0.00 to 20.6 msec/day
41871     130/1942     99-160    OBC      Clk Adj fr 20.6 to 0.00 msec/day
41873     130/2230     99-161    ACRIM    Power OFF
41874     131/0006     99-162    MLS      Power ON
41876     131/0336     99-163    HRDI     Day only operations
41903     132/2228     99-164    OBC      Clk Adj fr 0.00 to 20.6 msec/day
41918     133/2246     99-165    HALOE    Power OFF
41919     134/0059     99-166    ACRIM    Power ON
41919     134/0059     99-167    WINDII   Power ON
41926     134/1126     99-168    PEM      AXIS 1&2 ON
41930     134/1747     99-169    PEM      PEM CALS

_______________________________________________________________

                               APPENDIX B
                  OUT-OF-LIMITS & ALERTS OCCURRENCES
                      Week ending 14 May 1999

MNEMONIC           STATE      DESCRIPTION                       ORBITS
---------          -----      ------------                      ------
WIISUTEMP          Y-LO     WINDII ISU Temp              41881-88
WIISUTEMP          Y-LO     WINDII ISU Temp              continuous
SORLGCTMP          Y-LO     Logic_Box Temperature        continuous


The following ALERT occurrences were detected:

MNEMONIC              DESCRIPTION                           ORBITS
---------             ------------                          ------
                       None this report period


_______________________________________________________________

                              APPENDIX C
                 CLOCK & SOLAR ARRAY RATE CORRECTIONS
                       Week ending 14 May 1999

                      CLOCK DRIFT RATE ADJUSTMENTS

     ORBIT            TIME                    CLOCK RATE CHANGE
     -----            ----                    -----------------
     41845     129/01:39 (08 May 99)     from 00.0 to 20.6 msec/day
     41871     130/19:42 (10 May 99)     from 20.6 to 00.0 msec/day
     41903     132/22:28 (12 May 99)     from 00.0 to 20.6 msec/day


                             APPENDIX D
                    UARS BATTERY PERFORMANCE DATA
                       Week ending 14 May 1999


     07 May 1999 - GMT Day 127 Beta = 26.0 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   -78.4/-100.8  -3.05/-4.31  +0.0/ +0.0    16.5    0.000    0.0
2   +39.2/-16.8   +6.11/+4.83 +30.4/-15.2    24.8    1.023   22.1
3   +22.4/-50.4   +5.15/+3.87 +30.4/-16.0    24.8    1.024   22.0


     14 May 1999 - GMT Day 134 Beta = 55.9 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   -78.4/-112.0 -3.68/-4.94   +0.0/ +0.0    16.5    0.000    0.0
2   +22.4/-28.0  +5.15/+3.87  +24.8/-16.4    23.8    1.013   21.0
3   +22.4/-50.4  +4.51/+2.60  +24.8/-17.2    23.8    1.016   20.8


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



                               APPENDIX E
                         UARS ANOMALY REPORTS
                      Week ending 14 May 1999


                     NEW ANOMALY REPORTS GENERATED
  AR NO.  SUBSYS   ORBIT      TIME       TTR     PROBLEM/DATA LOSS
  ------   ------  -----      ----       ---     -----------------
99-026    HRDI    41875    131/0148     N/A    Not in Day Only as Scheduled
99-023    FOT     41929    134/1604    14170   Generic Late Acquisition


                  ANOMALY CLOSURE INFORMATION RECEIVED
  AR NO.  SUBSYS   ORBIT      TIME       TTR     PROBLEM/DATA LOSS
  ------  ------   -----      ----       ---     -----------------
99-024    FOT     41741    122/0302     20809  Late Acquisition
99-026    HRDI    41875    131/0148      N/A   Not in Day Only as Scheduled


                ANOMALY INVESTIGATION REPORTS GENERATED
  AIR NO.  SUBSYS   ORBIT     TIME       TTR     PROBLEM/DATA LOSS
  -------  ------   -----     ----       ---     -----------------
                      None this report period


                      OPEN ANOMALY REPORTS
  AR NO.   SUBSYS    ORBIT      TIME       TTR      PROBLEM/DATA LOSS
  ------   ------    -----      ----       ---      -----------------
99-023     FOT     see list     May 99     14170     Generic Late Acq

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