UARS Weekly Status Report

22 May 1998





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                UARS WEEKLY STATUS REPORT - 22 MAY 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.  

SOLSTICE science production software v. 4.61 has been promoted to
production, and mission reprocessing of our new v. 10 data products
is underway.

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

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

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

PEM/AXIS was active from May 10 through May 15 and became active again
on May 21.  It is currently generating energy deposition from inverted X-ray 
spectra for each of its 16 look directions.  The zenith boom instruments of PEM
we active from May 16 through May 20.  While active, they generated energy
deposition profiles from in situ measured electrons and ions.

GSFC has proposed an OBC operation plan for the activation of PEM boom 
instruments during the daylight portions of every orbit.  This OBC operation 
plan is accepted by PEM.  PEM has proposed a series of test procedures for 
activation and is waiting response from GSFC.  PEM is also waiting for GSFC
scheduling and implementation of the OBC plan and its operation test procedures.

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

HALOE was powered off May 19, 1998.  All engineering parameters were
nominal and science channel outputs were within expected operating range.
HALOE is scheduled to be powered on June 2, 1998.

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

MLS was reactivated successfully on May 20, in the reduced 85 watt power mode.
MLS instrument operations have continued flawlessly.  MLS is scheduled to
operate through June 1.

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

Nothing received.

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

Nothing received.

***********
MPG
***********

Routine processing of instrument Daily Activity Plans continues 
with no other problems.  The MPG continues to assist the Project 
Scientist with the scheduling of instrument operations.

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

The CDHF UCSS release 10.0 has been scheduled for May 27th and should require
about 10 hours of downtime during day shift. Users were requested to send
comments, reservations, or impact statements to the PAC account.

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.           
                  25 days PEM (3.32) PROD (1379R-1263C=116L)
                  67 days HAL (4.80) PROD (L1) (1868R-190C-2F=1676L)
                   1 day  HAL (4.80) PROD (L3) (1868R-1C=1867L)
 
The CDHF plans to utilize the UCSS Scheduler enhancement (New Expansion
Tool).  (PROBLEM REPORT 3427 generated 17-Jan-1997).
Currently jobs are automatically expanded every hour.  This new tool will  
be added to a production reprocessing DCL runstream which will speed up the
reprocessing by expanding at the completion of a job.  This tool will be used
based on the requirements of the PI and how much data can be handled at the
RAC's. The CDHF will continue to use the current automatic expansion task for
all other production processing.
                   
CDHF pending software upgrades: IDL 5.1, OpenIngres, UCSS.

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

REPORTING PERIOD

This report covers 09 May 1998 (Orbit 36379, GMT Day 129) through 15 May 
1998 (Orbit 36483, GMT Day 135).


SPACECRAFT OPERATIONS

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
         HALOE     129/0248     36380     On
          PEM      130/0104     36394     AXIS on
         WINDII    130/2339     36408     On
          PEM      135/2346     36483     AXIS off

The beta angle reached a minimum angle of 0.0 degrees on 05 May 1998 (DOY 
125).  The beta angle is now increasing toward a maximum angle of 78.0 
degrees on 26 May 1998 (DOY 146).

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 25.1 V end-of-night (EON) load bus voltage.  
Battery temperatures are stable with a temperature delta between Battery 2 
and Battery 3 of 1.1 degrees C.  Additional battery performance data for 
each battery on 09 May 1998 and 15 May 1998 are provided in Appendix D.

The clock error ranged from -10.2 to +10.6 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          =   none
%     OUT-OF-LIMITS   =   04

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

%     FOT     03
%     HALOE   02
%     PEM     02
%     WINDII  01

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

%     FOT     01

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

TRANSPONDER FREQUENCIES:
     Transponder A:  98/062  -  2287.496945
     Transponder B:  98/062  -  2287.497010


GROUND SYSTEM OPERATION

No (0) 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 98/127 show the observatory data loss to be 
20 hours, 43 minutes, 11.156 seconds.  This is a 0.0357 percent data loss 
which equals a 99.9643 percent data capture for the mission.

The FOT made several minor modifications to the OBCSTF resident POCC 
database this week.  The FOT will spend the next several weeks testing 
database 67 and making any further necessary corrections.

Identified a potential problem with the new AP software (10.11) during 
flight software testing.  This software was tested during the previous week 
and found to support the new flight software configuration.  However, the 
new AP software was modified to only support the new flight software, and 
is not compatible with the existing flight software configuration.  The AP 
software should support both configurations, so the transition to the new 
flight software can be made without the need to change ground software 
simultaneously.  Modification of the AP software to support all flight 
software configurations is being pursued.


OTHER SIGNIFICANT EVENTS

Continued testing of the upgrade to the OBC Power Monitor (PMON) flight 
software.  Minor changes to both the flight software and supporting ground 
database were made during the week.  Testing continues to proceed 
successfully.

Work continues on the UARS August orbit adjust planning.

FOT continues to support CNMOS in their efforts to make necessary software 
changes (MSOCC, CMS, DCF, etc.) to support the year 2000 rollover.

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.  
A response to a list of questions was prepared for distribution this week.


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 June 1998.

The UARS orbit altitude is dropping slowly and a drag makeup orbit adjust 
is targeted for 05 August 1998.


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 15 May 1998

ORBIT      AOS        NO.      SUBSYS       REASON
-----      ---        ---       ---         -------  
36380    129/0248    98-158     HALOE     Power ON
36394    130/0104    98-159     PEM/AXIS  Power ON
36408    130/2339    98-160     WINDII    Power ON
36415    131/1042    98-161     OBC       Clk Adj 0.0 to 20.6 msec/day
36435    132/1846    98-163     OBC       Clk Adj 20.6 to 0.0 msec/day
36440    133/0301    98-164     HALOE     CMDs to reset elevation position
36469    135/0125    98-165     OBC       Clk Adj 0.0 to 20.6 msec/day
36483    135/2346    98-166     PEM       Power OFF AXIS




_______________________________________________________________

                               APPENDIX B
                  OUT-OF-LIMITS & ALERTS OCCURRENCES
                      Week ending 15 May 1998

MNEMONIC       STATE        DESCRIPTION                ORBITS
---------      -----        ------------               ------
HRPSEQBIMON    Y-HI     HRDI QB Current Monitor     36398,36404,36413
QTSISAIF       Y-HI     SSPP Baseplate by SISA I/F  36379-36413
WIEUTEMP       Y-LO     WINDII EU Temperature       36379-36408
SOSTMPRNTRN    Y-LO     Temperature Entrance        36404,36480


The following ALERT occurrences were detected:

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



                               APPENDIX C
                 CLOCK & SOLAR ARRAY RATE CORRECTIONS
                      Week ending 15 May 1998

                      CLOCK DRIFT RATE ADJUSTMENTS

     ORBIT              TIME                 CLOCK RATE CHANGE
     -----              ----                 -----------------
     36415     131/10:47 (11 May 98)     from 00.0 to 20.6 msec/day
     36435     132/18:58 (12 May 98)     from 20.6 to 00.0 msec/day
     36469     135/01:29 (15 May 98)     from 00.0 to 20.6 msec/day


_______________________________________________________________

                               APPENDIX D
                    UARS BATTERY PERFORMANCE DATA
                      Week ending 15 May 1998

     09 May 1998 - GMT Day 129 Beta = 15.0 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   +728.0/+728.0  -3.05/-4.94    +0.0/ +0.0   18.4   0.000     0.0
2   +100.8/  +0.0  +6.44/+3.87   +31.2/-16.0   23.8   1.020    23.2
3    +67.2/  -5.6  +5.15/+2.60   +30.4/-16.4   23.8   1.019    22.4

     15 May 1998 - GMT Day 135 Beta = 40.7 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   18.4   0.000     0.0
2   +56.0/ -11.2   +6.11/+4.51   +28.8/-16.0   25.1   1.023    22.5
3   +67.2/  -5.6   +5.15/+3.55   +28.0/-16.0   25.1   1.024    21.9


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



                               APPENDIX E
                         UARS ANOMALY REPORTS
                      Week ending 15 May 1998


                    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
  ------   ------       -----      ----       ---      -----------------
98-021      Generic Late Acq for May 1998 (Open until 31 May 1998).



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