UARS Weekly Status Report

10 August 2001




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                UARS WEEKLY STATUS REPORT - 10 AUG 2001

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

SOLSTICE began a period of day only operations this week (Aug) insupport of
the yaw maneuver. We expect to return to normal operations at the end of
today (Aug 10) Otherwise, SOLSTICE continues to operate normally, taking 
solar data on all available orbital tracking periods and stellar calibration 
observations whenever possible. We continue to gather enough data to meet all 
the SOLSTICE science objectives during this period of reduced tape recorder 
operations.

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

On first examination, our lamp calibrations and reference channel scans
were performed successfully.  There was time for 3 of our 4 lamps.
Because additional experiment time was made available until Aug. 27,
we will be able to get the scan of the 4th lamp, completing our "end
of mission" calibration.  Additionally, SUSIM has completed its daily
solar scans this past week during periods of predicted UARS telemetry.

We have begun CDHF reprocessing hoping to finish before Oct. 1.  At the
present rate, it won't be completed.

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

Nothing received.

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

***** ALL PEM COMMUNICATION SHOULD NOW BE THROUGH THE PEM2K:: NODE *****

     PEM/AXIS was activated in activated in full power mode on July 27 and 
deactivated on August 4.  At the current time, AXIS is not generating energy 
deposition.  SwRI is looking into this.  Tests of AXIS production code on the 
rehost computer are continuing.

     At the present time, PEM energy deposition from its spectrometers 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 may include changes 
which would allow the PEM software to execute on a DEC Alpha machine.  GSFC is
helping PEM with some DEC Alpha particulars which have caused PEM level 3
code to fail on DEC Alpha machines (software below level 3 executes on the
DEC Alpha).

    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.

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

Nothing received.

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

Nothing received.

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

Nothing received.

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

Nothing received.

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

Daily processing of instrument Daily Activity Plans 
continues with no problems.

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

Nothing received.
                  
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FOT
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                         REPORTING PERIOD

This report covers 28 July 2001 (Orbit 54001, GMT Day 209) through 03 August 
2001 (Orbit 54105, GMT Day 215).

                        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

               -None this report period


The beta angle ranged between the angles of 49.9 degrees to 24.4 degrees for 
this report period.  The beta angle is now decreasing towards a minimum angle 
of 2.0 degrees on 8 August 2001 (DOY 220).

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 1.3 to 1.6 degrees C.  Additional battery performance data for each 
battery on 27 July 2001 and 03 August 2001 are provided in Appendix D.

The clock error ranged from Ð11.5 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   =  00
¥     ALERTS          =  00

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

¥     FOT             =  12


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:  00/316  - 2287.496493
· Transponder B:  01/119  - 2287.499116


                     GROUND SYSTEM OPERATION

One (1) 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 01/207 show the observatory data loss to be 302 hours, 55 
minutes, 48.256 seconds. This shows a loss of zero 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.


                     OTHER SIGNIFICANT EVENTS

                     UARS SATELLITE OPERATIONS

UARS continues under the direction of no funding for science after 30 September 
2001.  In order to prepare for possible deorbit maneuvers, UARS will prime the 
propulsion system starting next week.  The A-C attitude thrusters will be fired 
on Tuesday 07 August 2001, followed by B-D translation burns on both 08 and 09 
August 2001.  The translation burns will take place after Wednesday yaw 
maneuver and will be approximately 4 and 13 seconds in duration.  All 
instruments will be asked to verify proper configuration before burns will be 
executed.

                              MEETINGS

The UARS FOT attended a UARS EOM Planning Meeting on Tuesday, July 31,2001.
The UARS FOT attended a UARS Monthly Status Meeting on Wednesday, August 
01,2001.
The UARS FOT attended a 3 TDRS Meeting on Wednesday, August 01,2001.
The UARS FOT attended a Safehold Working Group Meeting on Thursday, August 02, 
2001.
The UARS FOT attended a Ground Rehost Demo Meeting on Thursday, August 02, 
2001.


                     FUTURE SIGNIFICANT EVENTS

The next UARS Yaw slew is scheduled for 08 August 2001 (DOY 220).  This 
maneuver will be a Forward to Reverse Flight maneuver (Southern 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 03 August 2001

ORBIT     AOS         NO.        SUBSYS     REASON
-----     ---         ---        ------     ------
54012     209/1811    01-479     NBTR       NOOPS D210
54024     210/1352    01-480     OBC        Clk Adj fr 0.00 to 20.6 msec/day
54027     210/1812    01-481     NBTR       NOOPS D211
54042     211/1814    01-482     NBTR       NOOPS D212
54043     211/2035    01-483     OBC        Clk Adj fr 20.6 to 0.00 msec/day
54057     212/1816    01-484     NBTR       NOOPS D213
54072     213/1817    01-485     NBTR       NOOPS D214
54086     214/1714    01-485     NBTR       NOOPS D214
54087     214/1820    01-486     NBTR       NOOPS D215
54095     215/0621    01-486     NBTR       NOOPS D-215
54101     215/1715    01-486     NBTR       NOOPS D-215
54102     215/1822    01-487     NBTR       NOOPS D-216

______________________________________________________________________________

                              APPENDIX B
                  OUT-OF-LIMITS & ALERTS OCCURRENCES
                       Week ending 03 August 2
ATE     DESCRIPTION     ORBITS
--------     -----     -----------     ------
-None this report period     


The following ALERT occurrences were detected:

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


_______________________________________________________________________________

                              APPENDIX C
                  CLOCK & SOLAR ARRAY RATE CORRECTIONS
                        Week ending 03 August 2001

                       CLOCK DRIFT RATE ADJUSTMENTS

ORBIT     TIME         CLOCK RATE CHANGE
-----     -----        -----------------
54024     210/1354     Clk Adj fr 0.00 to 20.6 msec/day
54043     211/2038     Clk Adj fr 20.6 to 0.00 msec/day     

_______________________________________________________________________________

                              APPENDIX D
                      UARS BATTERY PERFORMANCE DATA
                        Week ending 03 August 2001


     27 July 2001 - GMT Day 208 Beta = 54.1 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   -3.68/-4.94   +0.0/+0.0      12.0     0.000     0.0
2    +11.2/-67.2     +4.51/+3.23   +24.8/-15.2    25.0     1.050     17.9
3    +22.4/-44.8     +3.55/+2.29   +24.0/-14.4    24.8     1.050     17.0


     03 August 2001 - GMT Day 215 Beta = 54.1 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      12.0      0.000     0.0
2    +16.8/-78.4     +6.11/+4.51   +29.2/-14.4    24.2      1.030     21.4
3    +22.4/-50.4     +5.15/+3.87   +28.8/-14.4    24.2      1.020     21.1


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

_______________________________________________________________________________

                                   APPENDIX E
                        UARS ANOMALY REPORTS
                       Week ending 03 August 2001

                      NEW ANOMALY REPORTS GENERATED
AR NO.     SUBSYS     ORBIT     TIME         TTR       PROBLEM/DATA LOSS
------     ------     -----     ----         ---       -----------------
01-046     FOT        54099     215/1312     14170     Generic Late Acquisition


                ANOMALY CLOSURE INFORMATION RECEIVED
AR NO.     SUBSYS     ORBIT     TIME         TTR       PROBLEM/DATA LOSS
------     ------     -----     ----         ---       -----------------
01-041     FOT        see list  July 01      14170     Generic Late Acquisition


                  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
------     ------     -----     ----         ---       -----------------
01-045     FOT        see list  August 01    14170     Generic Late Acquisition


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