UARS Weekly Status Report

16 January 1998





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                UARS WEEKLY STATUS REPORT - 16 JAN 1998

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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
scan data during this past week without apparent problems.

The half yearly calibration was successfully completed.  In the coming
week, we plan to run field-of-view calibrations of SUSIM's lower

A poster paper entitled "Ultraviolet Irradiance at Solar Minimum" by
members of the SUSIM team was presented to the Washington, DC meeting
of the American Astronomical Society last week.


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

     The PEM zenith spectrometers were powered January 4.  HEPS-2 microprocessor
errors did not clear and the HEPS-2 unit was shut down.  The HEPS-2 unit was 
restarted on January 5 successfully.  This type of problem has been seen before
and appears to be a symptom of being cold for a long period of time.  It is not
anticipated that this problem will occur under solar array control. On 
January 9, the PEM zenith instruments were shut down.  During the time the PEM 
zenith spectrometers are powered, PEM produced energy deposition profiles from 
electron and proton precipitation.

     PEM is awaiting evaluation by GSFC of its proposed activation procedure.
The minimal configuration for PEM AUX activation is the zenith VMAG, MEPS1, 
MEPS2, and HEPS1 units, only.  This configuration is driven by the capabilities 
of the spacecraft OBC and may increase if OBC program area increases.  PEM 
activation is proposed to be OBC driven when there exists plenty of power to 
operate PEM.  It is anticipated that the OBC will activate PEM on the daylight 
portions of every orbit.


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

Nothing received.

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


The MLS instrument has been powered off since Dec 27, 1997. MLS is scheduled to
begin north viewing operations on Jan 20, 1998.



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

Nothing received.

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WINDII
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WINDII WEEKLY REPORT FOR THE WEEK ENDING JAN. 16, 1998

WINDII is currently off, awaiting its next operating period
which is planned for Feb. 3 to 12. 


***********
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 has received a total of 360 CD-ROM requests as of
16-January-98. There were five orders received and five orders shipped.

The CDHF previewed DAAC data for HALOE, HRDI, PEM, NMC, and UKMO 
for the month of November 1997.   

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.           
                  1 day SUSIM (6.3) Test (1R-1C=0L)
                  2 days SOLSTICE (4.52) Test (2R-2C=0L)
                  25 days PEM (3.32) Prod (1350R-775C=575L)
                  3 days MLS (4.90) Test (3R-3C=0L)
            
The CDHF continues to work with NSI to develop a support plan for the 
entire UARSNET network, focusing on Instrument RACs first, redesign issues, 
and then the global user community.  

                  
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FOT
***********

This report covers 03 January 1998 (Orbit 34492, GMT Day 003) through 
09 January 1998.

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
     PEM      004/1516     34516     ZEPS on
     PEM      009/2327     34596     ZEPS off

The beta angle is decreasing toward a minimum angle of 0.0 degrees on 
16 January 1998 (DOY 016).

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 25.0 V end-of-night (EON) load bus voltage.  Battery temperatures 
are stable with a temperature delta between Battery 2 and Battery 3 of 1.3 
degrees C.  Additional battery performance data for each battery on 03 January 
1998 and 09 January 1998 are provided in Appendix D.

The clock error ranged from -10.9 to +10.7 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
%     HRDI    01
%     PEM     03

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

%     FOT     02

TRANSPONDER FREQUENCIES:
     Transponder A:  97/364 - 2287.496935
     Transponder B:  97/365 - 2287.499033


GROUND SYSTEM OPERATION

One (1) operational support problem(s) 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 98/008 show the observatory data loss to be 20 hours, 41 
minutes, 30.836 seconds (an increase of 06.144 seconds since last reported).  
This is a 0.0375 percent data loss which equals a 99.9625 percent data capture 
for the mission.

The increase of 6.144 seconds occurred over three days as follows:

7 a loss of 0.512 seconds on Day 005 due to a hit in the data,
7 a loss of 2.080 seconds on Day 006 due to a hit in the data,
7 a loss of 2.944 seconds on Day 007 due to insufficient overlap and a hit
 in the data, and 
7 a loss of 0.608 seconds on Day 008 due to a hit in the data.

No testing of the new CMS software release (R7B1V2) occurred this week.

Operational processing of level-0 telemetry analysis files continues in 
parallel on both the UMPGAL (new MPG Alpha machine) and CDHF computer systems.  
Production level-0 file transfers between CDHF and UMPGAL failed partially on 
07 January 1998 at approximately 02:00 UTC.  This was the only file transfer 
problem identified this week.

The UARS simulator's Q-channel line problem was corrected on 05 January 1998.  
Arrangements were made for NASCOM hardware support to be available to 
troubleshoot the problem. After an initial failure on 05 January, NASCOM 
support made corrections and successful Q-line channel dumps were obtained. 
Continuous successful dumps were obtained throughout the day on Monday and 
again on Tuesday.  The corrective action taken by NASCOM to correct this 
problem is not clear.


OTHER SIGNIFICANT EVENTS

Work on the upgrade of the OBC Power Monitor (PMON) software has been 
initiated.  This week has been focused on the redesign (i.e., PDL); however, 
coding is not expected to begin until next week.  The coding should be done 
within two weeks after that, provided no problems are encountered.  Another 
week or so is anticipated in order to complete database updates and testing.  
Uplink scheduling then becomes contingent upon the Applications Processor (AP) 
software changes to support the reduced-size Absolute Time Command Processor 
(ATCP).  In summary, the software will be ready for uplink by late February 
provided no unanticipated problems are encountered.

Monitoring of the magnetic field model performance continues.

FOT continues to improve a Power Profile for UARS based on the current status 
of the Modular Power System.

FOT continues to support the new UARS ground system re-engineering effort.

All of the 1997 Anomaly Reports have been processed to closure.


MEETINGS

No UARS Battery telecon was held this week.  The next telecon has not been 
scheduled.


FUTURE SIGNIFICANT EVENTS

The next UARS Yaw Around Maneuver is currently scheduled for 16 January 1998 at 
016/13:25:18 UTC.

The UARS orbit altitude is dropping slowly and a drag makeup orbit adjust will 
probably be required in mid-1998.


FACILITIES

no change


PERSONNEL CHANGES

no change


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 09 January 1998

ORBIT      AOS         NO.    SUBSYS                REASON
-----      ---        ---     ------                -------  
34506    003/2328    98-002     HRDI    Power OFF
34507    004/0043    98-003     PEM     Power ON
34516    004/1516    98-004     PEM     Power ON HEPS 2
34517    004/1650    98-005     OBC     Clk Adj fr 20.6 to 0.00 msec/day
34550    006/2158    98-006     OBC     Clk Adj fr 0.00 to 20.6 msec/day
34576    008/1530    98-007     OBC     Clk Adj fr 20.6 to 0.00 msec/day
34596    009/2327    98-009   PEM/ZEPS  Power OFF


_______________________________________________________________

                               APPENDIX B
                  OUT-OF-LIMITS & ALERTS OCCURRENCES
                      Week ending 09 January 1998

  MNEMONIC      STATE           DESCRIPTION               ORBITS
  ---------     -----           ------------              ------
HRIFESURVTMP    Y-HI     HRDI IFE SURVIVAL HTR TEMP     34508     
QTSISAIF        Y-HI     SSPP Baseplate by SISA I/F     34579,93-6


The following ALERT occurrences were detected:

MNEMONIC                       DESCRIPTION                ORBITS
---------                      ------------               ------
                         (none this report period)



                               APPENDIX C
                 CLOCK & SOLAR ARRAY RATE CORRECTIONS
                      Week ending 09 January 1998

                      CLOCK DRIFT RATE ADJUSTMENTS

     ORBIT             TIME                 CLOCK RATE CHANGE
     -----             ----                 -----------------
     34517     004/16:54 (04 Jan 98)     from 20.6 to 00.0 msec/day
     34550     006/22:04 (06 Jan 98)     from 00.0 to 20.6 msec/day
     34576     008/15:33 (08 Jan 98)     from 20.6 to 00.0 msec/day


_______________________________________________________________

                
 January 1998

     03 Jan 1998 - GMT Day 003 Beta = 33.4 deg, SA Pos = 269 deg
E
BAT    MAX/MIN       MAX/MIN      MAX/MIN      MIN     RATIO   DOD(%)
---  --
------  -------  -------  ------
1  +728.0/+728.0  -2.73/-3.99   +0.0/ +0.0    18.6    0.000    0.0
2   +11.2/ -50.4  +6.44/+5.15  +31.2/-16.0    25.1    1.026    22.4
3   +33.6/ -22.4  +5.15/+3.87  +29.6/-16.0    25.0    1.026    21.7

     09 Jan 1998 - GMT Day 009 Beta = 22.8 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  +728.0/+728.0  -3.05/-4.31   +0.0/ +0.0   18.6    0.000     0.0
2    +5.6/ -67.2  +6.44/+5.15  +32.4/-15.2   25.0    1.027    22.8
3   +67.2/ -11.2  +5.15/+3.87  +31.2/-16.0   24.8    1.023    22.2


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

_______________________________________________________________
                               APPENDIX E
                         UARS ANOMALY REPORTS
                      Week ending 09 January 1998

  AR NO.   SUBSYS   ORBIT       TIME       TTR      PROBLEM/DATA LOSS
  ------   ------   -----       ----       ---      -----------------
98-001     FOT     34517     004/1650    14170    Generic Late Acquisition
98-003     FOT     34543     006/1006     N/A     TAC Crashed


             ANOMALY CLOSURE INFORMATION RECEIVED
  AR NO.   SUBSYS   ORBIT       TIME       TTR      PROBLEM/DATA LOSS
  ------   ------    -----      ----       ---      -----------------
97-124     FOT    (EIGHT)    DEC 97      14170    DEC. GEN LATE ACQ SUM
97-127     FOT     34207    349/00:18             GYRO GLITCH
97-128     FOT     34442    364/16:28             TAC CRASH
97-129     FOT     34444    364/20:03             TAC CRASH
97-130     FOT     34457    365/16:10    19647    TAC CRASH

          (END 1997 AR DATA - ALL 1997 AR CLOSED)

98-002     FOT     34465    001/07:14             TAC 2 CRASH
98-003     FOT     34563    006/10:06             TAC 4 CRASH


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