UARS Weekly Status Report

11 August 2000




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                UARS WEEKLY STATUS REPORT - 11 AUG 2000

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

SOLSTICE is in good health, collecting solar data on all available
orbital tracking periods and stellar calibration observations whenever
possible. The solar data is not affected by the larger than normal
pointing errors since they are within our calibrations. Additionally, we
continue to gather enough data to meet all the SOLSTICE science
objectives during this period of reduced tape recorder operations.
Level2 processing is halted due to bugs in the OA_SSPP_ATT service. CDHF
and CSC personnel are working on the problem.

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

Most of the daily data for August 8 were lost due to the UARS OBC ATC
halt.  The solar pointing, degraded due to the loss of the star tracker
has improved recently to a few arcmin.  Otherwise, SUSIM continues to
gather a normal set of daily solar scans scheduled for periods of
predicted telemetry.

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

The ACRIM II instrument is performing normally, producing high quality 
data. The decreased  SSPP pointing accuracy remains well within ACRIM II's 
tolerance and no significant degradation of results is anticipated. Data 
re-processing is under way using algorithm improvements derived from the 
ACRIMSAT/ACRIM III experiment. The long term record of ACRIM II results 
will be brought up to date this fall following completion of the re-processing.

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

     PEM/AXIS-1 was activated on July 27 and deactivated on July 22.  The
full PEM/AXIS was activated July 24 and deactivated July 26.  The PEM 
zenith spectrometers were reactivated in daylight mode on July 21.  All of
PEM was off for the July 12 particle event.

     At the present time, PEM energy deposition is not being generated.  
Recent data configuration changes have affected PEM software causing multiple 
failures.  These failures are being reviewed by the PEM team.  In order to 
correct for new telemetry requirements, PEM will need to update processing 
code with a patch delivery.  The delivery patch will not include changes which
would allow the PEM software to execute on a DEC Alpha machine.

    Updated HEPS calibration parameters have been finalized and are ready for 
delivery.  Updated MEPS quality calibration files have been finalized and are 
ready for delivery.  Level 3 software errors, discovered by Dr. Dean Pesnell, 
have been fixed; his suggestions have been incorporated with in the PEM 
production code.  Both updated HEPS and MEPS calibration data, along with the 
Level 3 code changes, will influence the in-situ energy deposition predictions,
so new versions of PEM energy deposition Level 3 files will be generated.

*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 
***********

Nothing received.

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MLS
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Nothing received.

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

Nothing received.

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

Nothing received.

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

Processing of instrument Daily Activity Plans continues with no
problems. We are continuing to coordinate with the Flight Operations
Team and to assist the Project Scientist in scheduling of instrument
operations. 

The MPG attended a meeting on 10 August 2000 to discuss the progress of
ongoing efforts to improve UARS attitude control using Fixed Head Star 
Tracker 1 and the Fine Sun Sensor.   Status of planning for future use of a 
magnetic field model and the three-axis magnetometer for spacecraft attitude 
control was also discussed. 

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

Nothing received.
                  
***********
FOT
***********

                           REPORTING PERIOD

This report covers 29 July 2000 (Orbit 48542, GMT Day 211) through 04 August 
2000 (Orbit 48646, GMT Day 217).

                       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         212/1325      48565       On
     HALOE          214/2349      48601       On 

The beta angle ranged between the angles of 71.3 degrees to 48.3 degrees for 
this report period.  The beta angle is now decreasing toward a minimum angle of 
+2 degrees on 14 August 2000 (DOY 227).

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  28 July 2000 and 04 August 2000 are provided in Appendix D.

The clock error ranged from -13.1 to 12.4 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  =  00
¥     ALERTS         =  02

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

¥     FOT            =  20
¥     WINDII         =  01
¥     HALOE          =  01

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

¥     FOT            =  02

Four (4) Anomaly Reports remained OPEN at the end of this report period (see 
Appendix E).

TRANSPONDER FREQUENCIES:
· Transponder A:  00/145  -  2287.497008
· Transponder B:  00/152  -  2287.498920

    
                     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 00/216 show the observatory data loss to be 296 hours, 54 
minutes, 26.417 seconds (an increase of 10 minutes 21.712 seconds since the 
last report period).  This is a 0.39 percent data loss which equals a 99.61 
percent data capture for the mission.

The increase of 10 minutes 21.712 seconds occurred over three (3) days:

· 00 minutes 03.056 seconds on Day 210 due to a late acquisition,
· 10 minutes 18.080 seconds on Day 212 due to an incorrect vector,
· 00 minutes 00.576 seconds on Day 213 due to a data hit.


                      OTHER SIGNIFICANT EVENTS

                      UARS SATELLITE OPERATIONS

UARS continues to operate FHST-1 this week.  More updates to the scale factor 
were uplinked this week on 31 July, 02 August and 04 August 2000.  These 
updates are now being provided on Monday, Wednesday and Friday from FDF.  A 
star intensity calibration was also uplinked on 02 August 2000.  The FOT will 
continue to perform calibrations so that the FHST-1 is performing at its best 
for the yaw maneuver on 14 August 2000.  The star tracker is now being cycled 
on for one orbit each day to conserve its useful life.

The FOT has delayed the testing of the new TMONs until the FHST-2 anomaly is 
resolved.  No time frame has been set as to when testing will resume.

The FOT has begun writing the online procedure for safehold should it happen 
before the new TMONs are in place or during and OBC halt.  This procedure will 
be tested on the simulator and put online for immediate execution should an 
anomalous condition take place.

                               MEETINGS

The FOT attended a meeting to discuss FHST-1 on 02 August 2000.  The main 
action items from this meeting were to begin power cycling the star tracker, 
look into how accurate UARS can be with just the TAM and FSS and compare a 5th 
order magnetic field model with a 7th order model.

The FOT attended the monthly status meeting on 02 August 2000.


                      FUTURE SIGNIFICANT EVENTS

The next UARS Yaw slew is scheduled for August 14, 2000 (DO
ght 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 04 Aug 2000

 ORBIT     AOS          NO.        SUBSYS     REASON
 -----     ---          ---        ------     -------
48549     211/1146     00-373     OBC        Clk Adj fr 20.6 to 41.2 msec/day
48565     212/1325     00-374     WINDII     Power ON
48568     212/1825     00-375     OBC        Clk Adj fr 41.2 to 20.6 msec/day
48572     213/0126     00-376     OBC        Clk Adj fr 20.6 to 0.00 msec/day
48584     213/2011     00-377     FHST1      SCALE FACTOR UPDATE
48598     214/1917     00-379     OBC        Clk Adj fr 0.00 to 20.6 msec/day
48601     214/2349     00-380     HALOE      Power ON
48605     215/0631     00-378     NBTR       NOOPS D-215
48613     215/1832     00-381     NBTR       NOOPS D-216
48613     215/1832     00-382     FHST-1     Intensity Calibration
48615     215/2207     00-383     FHST-1     Scale Factor Update
48619     216/0353     00-383     MACS       FHST 1 POWER OFF
48620     216/0534     00-381     NBTR       NOOPS D-216
48625     216/1414     00-383     MACS       FHST-1 POWER ON
48626     216/1555     00-385     MACS       FHST-1 POWER OFF
48628     216/1834     00-384     NBTR       NOOPS D-217
48626     216/1914     00-386     OBC        Clk Adj fr 20.6 to 0.00 msec/day
48634     217/0355     00-387     FHST-1     Power ON
48635     217/0535     00-387     FHST-1     Power OFF
48641     217/1556     00-388     FHST-1     Power ON
48642     217/1736     00-388     FHST-1     Power OFF
48643     217/1837     00-389     NBTR       NOOPS D-218
48644     217/2058     00-390     FHST/OBC   Scale Factor Update 
______________________________________________________________________________
                                 
                                   APPENDIX B
                       OUT-OF-LIMITS & ALERTS OCCURRENCES
                           Week ending 04 Aug 2000

The following Out-Of-Limits occurrences were detected:

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

The following ALERT occurrences were detected:
 
 MNEMONIC       DESCRIPTION                               ORBITS
 ---------      ------------                              ------
 OBSZ1OOL       UFLTR Z1 Residual Exceeded 100 Arcsec     Continuous
 OBSZ2OOL       UFLTR Z2 Residual Exceeded 100 Arcsec     Continuous

_______________________________________________________________________________

                                   APPENDIX C
                       CLOCK & SOLAR ARRAY RATE CORRECTIONS
                             Week ending 04 Aug 2000

                          CLOCK DRIFT RATE ADJUSTMENTS

  ORBIT     TIME                            CLOCK RATE CHANGE
  -----     ----                            -----------------
  48549     211/11:46 (29 July 00)         from 20.6 to 41.2 msec/day
  48568     212/18:34 (30 July 00)         from 41.2 to 20.6 msec/day
  48572     213/01:33 (30 July 00)         from 20.6 to 00.0 msec/day
  48598     214/19:17 (01 Aug 00)          from 00.0 to 20.6 msec/day
  48626     216/19:26 (03 Aug 00)          from 20.6 to 00.0 msec/day
_______________________________________________________________________________

       
              UARS BATTERY PERFORMANCE DATA
                           Week ending 04 Aug 2000


     28 July 2000 - GMT Day 210 Beta = 71.3 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    +67.2/+44.8     -2.42/-3.68   +0.0/+0.0      15.5      0.000     0.0
2    +16.8/-11.2     +3.23/+1.66   +17.6/-13.6    27.0      1.028     14.8
3    +22.4/-22.4     +2.60/+1.34   +16.8/-13.6    27.0      1.030     14.5


     04 Aug 2000 - GMT Day 217 Beta = 48.3 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    +78.4/+56.0    -3.05/-4.31   +0.0/+0.0      15.5       0.000     0.0
2    +44.8/-33.6    +5.79/+4.19   +27.2/-15.2    25.0       1.020     21.6
3    +22.4/-44.8    +4.51/+3.23   +26.8/-15.2    24.8       1.020     21.2


     V/T LEVEL CHANGES
   ORB#      TIME           LVL FR-TO
   -----     ----------     ----------
             no changes     V/T 5
______________________________________________________________________________
                                    APPENDIX E
                               UARS ANOMALY REPORTS
                              Week ending 04 Aug 2000

                          NEW ANOMALY REPORTS GENERATED
AR NO.     SUBSYS     ORBIT     TIME        TTR       PROBLEM/DATA LOSS
------     ------     -----     ----        ---       -----------------
00-034     FOT        48566     212/1547    22739     No Lock/Bad Vector
00-035     FOT        48649     218/0455    22770     Dropouts/Ret. Link

                      ANOMALY CLOSURE INFORMATION RECEIVED
AR NO.     SUBSYS     ORBIT     TIME        TTR       PROBLEM/DATA LOSS
------     ------     -----     ----        ---       -----------------
00-033     FOT        48509     208/1958    2723      Late Acq.

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

                              OPEN ANOMALY REPORTS
AR NO.     SUBSYS     ORBIT     TIME        TTR       PROBLEM/DATA LOSS
------     ------     -----     ----        ---       -----------------
00-026     FOT        see list  June 00     14170     Generic Late Acq.
00-032     FHST       48211     188/2242    N/A       FHST 2 Anomaly
00-034     FOT        48566     212/1547    22739     No Lock/Bad Vector
00-035     FOT        48649     218/0455    22770     Dropouts/Ret. Link

	 	SEVNTFW00/31