UARS Weekly Status Report

28 March 2003




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                UARS WEEKLY STATUS REPORT - 28 March 2003

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

SOLSTICE continues to perform nominally, taking solar data on all
available orbital tracking periods.

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

SUSIM successfully gathered all of its daily mid resolution, weekly
offset, and occultation scans during periods of UARS telemetry.

The data integrity problems of NRT and other files copied
from the CDHF was found to be due to a problem in the networking
infrastructure at NRL.  Many thanks to Mike Anderson of the CDHF
for his help in solving the problem.

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

Nothing received.

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

Nothing received.

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

Nothing received.

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

Nothing received.

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

Nothing received.

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

Nothing received.

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

The MPG continues to serve as the point-of-contact for UARS
instrument operations in support of the Science Traceability
Mission of UARS.

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

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

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

                           REPORTING PERIOD

This report covers 15 March 2003 (Orbit 62939, GMT Day 074) through 21
March 2003 (Orbit 63043, GMT Day 080).


                         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
       AXIS 1,2      077/1347      62993     POWER ON


The  beta  angle  ranged between the angles of 51.9  degrees  to  56.6
degrees  for  this  report period.  The beta angle is  now  decreasing
towards a minimum angle of 0 degrees on 06 April 2003 (DOY 096).

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 23.6 V end-of-night (EON) load  bus
voltage.   Battery  temperatures are stable with a  temperature  delta
between Battery 2 and Battery 3 of 1.26 to 1.27 degrees C.  Additional
battery  performance data for each battery on 14 March  and  21  March
2003 are provided in Appendix D.

The  clock  error  ranged from -10.4 to 10.9 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       =    04
    PEM       =    01

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

    FOT  =    00

Three  (3)  Anomaly  Reports remained OPEN at the end  of  this  
report period (see Appendix E).


                        GROUND SYSTEM OPERATION

Zero  (0) operational support problems occurred this period.   Anomaly
Reports are included in Appendix E.

The  data  loss  calculations are no longer  being  supplied  by  Data
Capture Facility (DCF).


                       OTHER SIGNIFICANT EVENTS


                       UARS SATELLITE OPERATIONS


The FOT began testing the new software release of the Eclipse software
(Version 2.1).  This release contains several fixes in response to DRs
written, including wait statement and status buffer issues.  Testing
showed that both the wait statement and status buffer problems had not
been fixed, so the Raytheon development team has been informed and
they will try to give us an updated build as soon as possible.


                               MEETINGS

-The FOT attended a PACOR-A meeting to discuss the processing of the 1
Kbps engineering data stream.


                       FUTURE SIGNIFICANT EVENTS

The next UARS Yaw slew is scheduled for 06 April 2003 (DOY 096).  This
maneuver  will  be  a  Reverse to Forward  Flight  maneuver  (Southern
Hemisphere viewing).






Attachments:   Appendix A,     Real-time Command 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 21 March 2003


ORBIT   AOS        NO.      SUBSYS      REASON
-----   ---        ---      ------      ------
62943   074/0705   03-064   OBC/CLK     CLK ADJ FR 20.6 TO 0.0 MSEC/DAY
62978   076/1457   03-065   OBC/CLK     CLK ADJ FR 0.0 TO 20.6 MSEC/DAY
62993   077/1347   03-066   AXIS 1,2    POWER ON
63010   078/1717   03-067   OBC         CLK ADJ FR 20.6 TO 0.0 MSEC/DAY
63038   080/1448   03-068   OBC/CLK     CLK ADJ FR 0.0 TO 20.6 MSEC/DAY



                              APPENDIX B
                  OUT-OF-LIMITS & ALERTS OCCURRENCES
                       Week ending 21 March 2003

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
--------     -----------                          ------
-None this report period.




                              APPENDIX C
                 CLOCK & SOLAR ARRAY RATE CORRECTIONS
                       Week ending 21 March 2003

                     CLOCK DRIFT RATE ADJUSTMENTS

ORBIT          TIME                   CLOCK RATE CHANGE
-----          -----                  -----------------
62943          074/0708               CLK ADJ FR 20.6 TO 0.0 MSEC/DAY
62978          076/1503               CLK ADJ FR 0.0 TO 20.6 MSEC/DAY
63010          078/1717               CLK ADJ FR 20.6 TO 0.0 MSEC/DAY
63038          080/1452               CLK ADJ FR 0.0 TO 20.6 MSEC/DAY


                              APPENDIX D
                     UARS BATTERY PERFORMANCE DATA
                       Week ending 21 March 2003

     14 March 2003 - GMT Day 073 Beta = 47.9 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  -168.0/-190.4  -3.05/-4.31  +00.0/+00.0  08.3     0.000     0.0
2   +11.2/-140.0  +5.47/+3.87  +25.6/-16.0  24.8     1.030    20.2
3   +24.0/-44.8   +4.51/+2.92  +25.2/-16.0  24.8     1.030    19.8


     21 March 2003 - GMT Day 080 Beta = 56.6 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  -168.0/-190.4  -3.68/-4.94  +00.0/+00.0  08.3     0.000     0.0
2   +11.2/-44.8   +4.19/+2.92  +23.2/-15.2  25.9     1.020    19.0
3   +22.4/-22.4   +3.23/+1.97  +22.4/-15.2  25.9     1.010    18.5


     V/T LEVEL CHANGES
ORB#           AOS TIME   LVL FR-TO
-----          --------   ---------
-None this report period.



                              APPENDIX E
                         UARS ANOMALY REPORTS
                       Week ending 21 March 2003

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

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

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

                         OPEN ANOMALY REPORTS
AR NO.    SUBSYS    ORBIT     TIME      CDS       PROBLEM/DATA LOSS
------    ------    -----     ----      ---       -----------------
02-060    FOT       61421     338/0057  N/A       PSU Cmd Clock Timeout
03-005    FOT       62559     048/1757  32330     CDS Equipment problem
03-007    FOT       62918     072/1352  N/A       Router Change / TLM hits