UARS Weekly Status Report

29 JANUARY 1999




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                UARS WEEKLY STATUS REPORT - 29 JAN 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 successfully gathered its normal solar, offset, and occultation
data without apparent problems.

Reprocessing of the SUSIM data to version 20 continues.

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

Nothing received.

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

Nothing received.

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

MLS was reactivated successfully on Jan 26 and is scheduled to operate though
Feb 11. The MLS team is operating the instrument in a mode emphasizing
scientific observations at the northern latitudes. 

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

HRDI continues to operate normally.

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

WINDII is currently on, and operating normally. It is expected to 
continue measurements until February 7. 

***********
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.
              0 days HAL (4.80) PROD (L3)    (1874R-1721C-1F=152L)
            147 days SUS (7.00) PROD (L3)    (2051R-1739C-9F=303L)
              3 days HAL (4.81) ENG (L1-L3)  (3R-3C=0L)
              0 days WIN (5.11) ENG (L1-L3)  (1R-1F=1L)
                                                    
Upgrades to UCSS10.1, UOAS5.4,  MSS4.1 and NRT 2.6 are completed.  A message 
pertaining to logical changes required by RACs using "nrt watch" 
programs was sent to UARS distribution.   

CDHF completed the upgrade of LSE to Version 4.5 and PCA to
version 4.5-4 as part of the ongoing Y2K implementation effort.

SOLSTICE Wall Clock time increase.-  Enough debug output has been produced to
enable tracking down the problem on the operational system where job step 2
takes an inordinate amount of time to complete. Steps are underway to create an 
engineering job for this purpose.

DAAC data created for HALOE, HRDI, NMC, PEM, and UKMO in the month
of November 1998 has been loaded into the DAAC Transfer Tables.

CDHF pending software upgrades: IDL 5.03(installed/not operational), 
OpenIngres, HALOE 4.81.  
                  
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FOT
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REPORTING PERIOD

This report covers 16 January 1999 (Orbit 40152, GMT Day 016) through 22 
January 1999 (Orbit 40255, GMT Day 022).


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
              PEM        022/2052     40254     PEM Test

The beta angle ranged between +14.6 degrees to 43.3 degrees for this report 
period. The beta angle is now increasing toward a maximum angle of 74.0 
degrees on 31 January 1999 (DOY 011).

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 15 January 1999 and 22 January 1999 are provided in 
Appendix  D.

The clock error ranged from -10.1 to 11.3 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.

%     ALERTS         = 00
%     OUT-OF-LIMITS  = 01

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

%     FOT     03
%     PEM     03

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

%     FOT     00

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

TRANSPONDER FREQUENCIES:
     Transponder A:  99/362  -  2287.496912
     Transponder B:  99/357  -  2287.499093


GROUND SYSTEM OPERATION

No (0) 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 99/021 show the observatory data loss to be 
21 hours, 50 minutes, 20.788 seconds (an increase of 16.480 seconds since 
last report period).  This is a 0.0340 percent data loss which equals a 
99.9660 percent data capture for the mission.

The increase of 16.480 seconds occurred over four (4) days:

7 2.048 seconds on Day 015 due to hit in data (IP),
7 9.696 seconds on Day 016 due to insufficient overlap,
7 1.120 seconds on Day 018 due to hit in data (IP), and
7 3.616 seconds on Day 019 due to insufficient overlap.

The UARS Test and Training Simulator (UTTS) remains non-operational.  The 
estimated time to repair the UTTS and return it to operation is unknown.


OTHER SIGNIFICANT EVENTS

UARS SATELLITE OPERATIONS

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 - No change


UARS PROPULSION MODULE B/D THRUSTER LINE FILL

Planning continues for the simulator testing.


UARS RE-ENGINEERING - TELEMETRY PROCESSING - No change


MEETINGS

The FOT attended a UARS Y2K end-to-end testing meeting on 20 January.  
Representatives of the various UARS related facilities (i.e. MSOCC, CDHF, 
IPD, etc) were in attendance.  As of this date, there are several entities 
that are not quite ready to participate in UARS Y2K end-to-end testing.  
One major show stopper for UARS is the current system disk problem with the 
UTTS.


FUTURE SIGNIFICANT EVENTS

The next UARS Yaw Around Maneuver is scheduled for scheduled for 20 
February 1999.


The next annular solar eclipse will occur on 16 February 1999 over the 
Indian Ocean, Australia and the South Pacific Ocean.


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 22 January 1999

ORBIT        AOS       NO.       SUBSYS      REASON
-----        ---       ---       ------      -------  
40166     016/2254     99-027     OBC     Clk Adj fr 20.6 to 0.00 msec/day     
40216     020/0745     99-028     OBC     Clk Adj fr 0.00 to 20.6 msec/day
40243     022/0158     99-029     PEM     HEP1 EPR ENA
40247     022/0940     99-030     OBC     Clk Adj fr 20.6 to 0.00 msec/day
40254     022/2052     99-031     PEM     Genascii
40254     022/2052     99-032     PEM     PMON Action 26

_______________________________________________________________

                               APPENDIX B
                  OUT-OF-LIMITS & ALERTS OCCURRENCES
                      Week ending 22 January 1999

MNEMONIC       STATE      DESCRIPTION                       ORBITS
---------      -----      ------------                      ------
HRPSEQBIMON     Y-HI     PSE Quiet Bus Current Mon     40205,15-17


The following ALERT occurrences were detected:

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


_______________________________________________________________

                              APPENDIX C
                 CLOCK & SOLAR ARRAY RATE CORRECTIONS
                       Week ending 22 January 1999

                      CLOCK DRIFT RATE ADJUSTMENTS

     ORBIT              TIME                 CLOCK RATE CHANGE
     -----              ----                 -----------------
     40166     016/22:59 (16 Jan 99)     from 20.6 to 00.0 msec/day
     40216     020/07:53 (20 Jan 99)     from 00.0 to 20.6 msec/day
     40247     022/09:43 (22 Jan 99)     from 20.6 to 00.0 msec/day


_______________________________________________________________


                             APPENDIX D
                    UARS BATTERY PERFORMANCE DATA
                       Week ending 22 January 1999


     15 Jan 1999 - GMT Day 015 Beta = 14.6 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/+22.4  -3.05/-4.62    +0.0/ +0.0   16.8    0.000    0.0
2  +112.0/+11.2  +7.09/+5.15   +32.0/-15.2   23.8    1.023   23.1
3   +22.4/-22.4  +5.47/+3.87   +31.6/-16.8   23.7    1.022   23.0


     22 Jan 1998 - GMT Day 022 Beta = 43.3 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   +39.2/+11.2  -3.05/-4.31   +0.0/ +0.0    16.8    0.000    0.0
2   +22.4/-50.4  +6.44/+4.51  +29.6/-16.0    25.1    1.023   22.1
3   +33.6/-11.2  +5.15/+3.87  +28.8/-16.0    25.1    1.026   21.8


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





                               APPENDIX E
                         UARS ANOMALY REPORTS
                      Week ending 22 January 1999


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


                  ANOMALY CLOSURE INFORMATION RECEIVED
  AR NO.   SUBSYS       ORBIT      TIME       TTR      PROBLEM/DATA LOSS
  ------   ------       -----      ----       ---      -----------------
                   None this report period


               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
  ------   ------       -----      ----       ---      -----------------
99-001      FOT     see list     Jan 98     14170     Generic Late Acq



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