UARS Weekly Status Report

31 DECEMBER 1999




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                UARS WEEKLY STATUS REPORT - 31 DEC 1999

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

We continue to gather enough data to meet all the SOLSTICE science
objectives during this period of reduced tape recorder operations. SOLSTICE
operates normally, collecting solar data on all available orbital tracking
periods and stellar calibration observations, whenever possible.

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

Nothing received.

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ACRIM
***********

Nothing received.

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PEM
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     The PEM team wishes everyone Happy Holidays!

     Daily activity plans for the PEM instrument were successfully generated
for the first two weeks of 2000.  PEM health and safety data monitoring, which
was reconfigured for day light operation, are being reviewed to determine
if they can be modified to account for telemetry dropouts caused by the tape 
recorder failure.  The PEM:: microVAX needs replacement as it is not Y2K
compliant.

     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.  

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

The CDHF continues to notify all PI Software Representatives when Data Gaps
occur in the LEVEL0 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.
        21 days GPI (4.05)  PROD (CLAES L3B)     (432R-419C-4F=9L)
        41 days WIN (5.11A) PROD (L1-L3)         (520R-230C-8F=282L)

UARS CDHF REHOST:                                                         
-  SUSIM has successfully validated the output products created on the
   Rehost System from the SUSIM V7.1 testing.
-  Testing HRDI V4.4 on the Rehost System.     
-  Testing SOLSTICE V4.62 on the Rehost System.

DAAC DATA
Data created in the month of October 1999 for HALOE, NMC, UKMO, and PEM has
been loaded into the DAAC Transfer Tables.  DAAC has been notified.
             
CDHF pending software upgrades: none 
                  
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FOT
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REPORTING PERIOD

This report covers 18 December, 1999 (Orbit 45185, GMT Day 352) through 24 
December 1999 (Orbit 45289, GMT Day 358).

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
               WINDII     357/2346   45274     Off

The beta angle ranged between the angles of 26.8 degrees to 33.2 degrees for 
this report period.  The beta angle is now decreasing toward a minimum angle of 
+1.0 degrees on 06 January 1999 (DOY 006).

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 17 December 1999 and 20 December 1999 are provided in Appendix D.

The clock error ranged from -12.3 to 10.2 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.

%     OUT-OF-LIMITS =   05
%     ALERTS        =   00

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

%     FOT           =   13
%     WINDII        =   01

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

%     FOT           =   06

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

TRANSPONDER FREQUENCIES:
%     Transponder A:  99/320  -  2287.496800
%     Transponder B:  99/334  -  2287.499196


GROUND SYSTEM OPERATION

Three (6) 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 99/357 show the observatory data loss to be 404 hours, 03 
minutes, 40.729 seconds (an increase of 61 hours 55 minutes 32.000 seconds 
since the last report period).  This is a 0.5586 percent data loss which equals 
a 99.4414 percent data capture for the mission.

The increase of 61 hours 55 minutes 32.000 seconds occurred over seven (7) 
days:

- 04 hours 34 minutes 58.688 seconds on Day 351 due to a S/C TR problem.
- 05 hours 45 minutes 37.248 seconds on Day 352 due to a S/C TR problem.
- 11 hours 30 minutes 11.072 seconds on Day 353 due to a S/C TR problem.
- 10 hours 01 minutes 24.448 seconds on Day 354 due to a S/C TR problem.
- 09 hours 56 minutes 52.960 seconds on Day 355 due to a S/C TR problem.
- 10 hours 10 minutes 50.176 seconds on Day 356 due to a S/C TR problem.
- 09 hours 55 minutes 37.408 seconds on Day 357 due to a S/C TR problem.


OTHER SIGNIFICANT EVENTS

UARS SATELLITE OPERATIONS

UARS completed a nominal 0.4 degree roll maneuver to return to normal pointing.
This finished up a request from WINDII for their science observations.  This 
return maneuver was completed Thursday, December 23, 1999 at 18:26:13 Z.

The FOT investigated a repeating low limit violation of the Communication and 
Data Handling current.  A low current alert was flaging during random 
spacecraft contacts.  After careful review it was determined that the low 
current limit violation was a result of the new tape recorder operations.  The 
tape recorder draws more current depending on which state it is in, either 
playback, record or standby.  More specifically, the tape recorder is in the 
standby mode during these low limit violations which consequently draws the 
least amount of current.  Previously the recorder was either in playback mode 
or recorder thus never violating the low current limit.

An action has been generated to lower the CDH current limit set to compensate 
for the new tape recorder management.

The FOT developed a tape recorder management plan.  This plan will be submitted 
for approval next week.


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

The FOT did not attend any meetings during this report period.


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.

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 January 6, 2000.  This maneuver will be 
a Forward to Reverse Flight maneuver (Northern 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 24 December 1999

ORBIT        AOS         NO.      SUBSYS   REASON
-----       ---          ---      ------   -------
45198     352/2139     99-421     NBTR     NOOPS
45213     353/2142     99-422     NBTR     NBTR NOOPS
45228     354/2226     99-423     NBTR     NBTR NOOPS
45239     355/1506     99-424     OBC      Clk Adj fr 0.00 to 20.6 msec/day
45241     355/1826     99-425     NBTR     NBTR RTS-58
45243     355/2149     99-426     NBTR     NBTR NOOPS
45258     356/2051     99-427     NBTR     NBTR NOOPS
45264     357/0712     99-427     NBTR     NBTR NOOPS
45261     357/0310     99-428     OBC      Clk Adj fr 20.6 to 0.00 msec/day
45270     357/1651     99-429     OBC      Roll Maneuver
45272     357/2053     99-430     NBTR     NBTR NOOPS
45274     357/2346     99-431     WINDII   Power OFF
45285     358/1736     99-430     NBTR     NBTR NOOPS
45286     358/1916     99-432     NBTR     NBTR NOOPS

___________________________________________________________________________
APPENDIX B
OUT-OF-LIMITS & ALERTS OCCURRENCES
Week ending 24 December 1999

The following Out-Of-Limits occurrences were detected:

MNEMONIC       STATE     DESCRIPTION                ORBITS
---------     -----      ------------               ------
HRPTSPBIMON    R-LO     PTS Pulse Bus Current Mon   45242
PWICDH         Y-LO     CDH CURRENT                 45242-46,56
PWICDH         Y-LO     CDH Current                 45269
PWICDH         Y-LO     CDH CURRENT                 45276,7,8
HRPTSPBIMON    Y-HI     PTS Pulse Bus Current Mon   45282-6

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 24 December 1999

CLOCK DRIFT RATE ADJUSTMENTS

ORBIT             TIME              CLOCK RATE CHANGE
-----             ----              -----------------
45239     355/15:11 (21 Dec 99)     from 0.00 to 20.6 msec/day
45261     357/03:13 (23 Dec 99)     from 20.6 to 0.00 msec/day

_______________________________________________________________________________

APPENDIX D
UARS BATTERY PERFORMANCE DATA
Week ending 20 December 1999

     17 Dec 1999 - GMT Day 351 Beta = 26.8 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   -44.8/-67.2     -2.73/-3.68   +0.0/+0.0    16.2      0.000     0.0
2   +39.2/-44.8     +7.09/+5.47  +31.2/-15.2   24.5      1.030    21.1
3   +33.6/-16.8     +5.79/+4.51  +30.8/-16.4   24.3      1.023    21.0

     20 Dec 1999 - GMT Day 354 Beta = 31.8 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   -44.8/-67.2     -3.05/-3.99    +0.0/+0.0    16.2     0.000     0.0
2   +22.4/-44.8     +6.11/+5.15   +30.4/-15.2   24.8     1.030    21.5
3   +44.8/-11.2     +5.15/+3.87   +29.6/-16.0   24.8     1.028    21.3

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


APPENDIX E
UARS ANOMALY REPORTS
Week ending 24 December 1999

NEW ANOMALY REPORTS GENERATED
AR NO.     SUBSYS   ORBIT     TIME      TTR     PROBLEM/DATA LOSS
------     ------   -----     ----      ---     -----------------
99-089     FOT     45188    352/0516    14170   Generic Late Acquisition
99-091     FOT     45190    352/0938    21717   Fwd link failure at WS
99-092     FOT     45226    354/1823    N/A     AP 8 Crashed
99-093     FOT     45256    356/1911    21745   White Sands S/W prob
99-095     FOT     45273    357/2157    N/A     AP2 Crash
99-096     FOT     45287    358/2015    21757   CSC Bad TDRSS Vectors

ANOMALY CLOSURE INFORMATION RECEIVED
AR NO.     SUBSYS   ORBIT     TIME      TTR     PROBLEM/DATA LOSS
------     ------   -----     ----      ---     -----------------
99-091     FOT     45190    352/0938   21717    Fwd link failure at WS
99-092     FOT     45226    354/1823   N/A      AP 8 Crashed
99-093     FOT     45256    356/1911   21745    White Sands S/W prob
99-095     FOT     45273    357/2157   N/A      AP2 Crash
99-096     FOT     45287    358/2015   21757    CSC Bad TDRSS Vectors

      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
99-089     FOT     45095    346/0123    14170    Generic Late Acquisition

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