UARS Weekly Status Report

31 October 2003




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                UARS WEEKLY STATUS REPORT - 31 Oct 2003

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

SOLSTICE continues to perform nominally, taking solar data on all
available orbital tracking periods. This week we received about 53% of
each day's data amounting to nearly 640 minutes of solar observing time
per day.

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

SUSIM successfully gathered all of its daily mid (1.1 nm)
resolution, weekly offset, and O2 occultation scans during periods
of UARS telemetry or periods of onboard tape recording.

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

Nothing received.

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

Nothing received.

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

Nothing received.

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

Nothing received.

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

Nothing received.

***********
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 18 October 2003 (Orbit 66202, GMT Day 291) through
24 October 2003 (Orbit 66306, GMT Day 297).


                         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          292/1230      66225     POWER ON AXIS 2


The  beta  angle  ranged between the angles of 60.7  degrees  to  67.3
degrees  for  this  report period.  The beta angle is  now  decreasing
towards a minimum angle of 0 degrees on 11 November 2003 (DOY 315).

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 1.58 degrees C.  Additional
battery performance data for each battery on 17 October and 24 October
2003 are provided in Appendix D.

The  clock  error  ranged from -10.5 to 09.8 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       =    03
    SUSIM     =    00
    SOLSTICE  =    00
    PEM       =    01
    HALOE     =    00
    HRDI      =    00



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).


                        GROUND SYSTEM OPERATION

One  (1)  operational support problem 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

Testing of the new 3 TDRS functionality on both the Eclipse and CMS
continued this week.  Raytheon provided a preliminary build, which was
installed on the prototype on 22 October 2003.  So far only two minor
problems have been found but will be fixed in the official build
delivery next week.  A few tests still need to be completed next week
in order to verify all functionality is working as planned.  A problem
was also found with the new CMS code, in regards to how the three TDRS
ephemeris load is built.  Software development is analyzing the
problem and will hopefully find a fix quickly.

In parallel, the FOT is also working with the FSW group to review and
test the new flight software uplink procedure.  Testing has gone well
so far and should be completed by the second week in November so that
the end-to-end testing can begin.



                               MEETINGS


-None this report period



                       FUTURE SIGNIFICANT EVENTS

The  next  UARS Yaw slew is scheduled for 11 November 2003 (DOY  315).
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 24 October 2003

ORBIT   AOS        NO.      SUBSYS      REASON
-----   ---        ---      ------      ------
66203   291/0220   03-277   OBC/CLK     CLK ADJ FR 0.0 TO 20.6 MSEC/DAY
66225   292/1230   03-278   AXIS        POWER ON AXIS 2
66261   294/2239   03-279   OBC/CLK     CLK ADJ FR 20.6 TO 41.2 MSEC/DAY
66288   296/1834   03-280   OBC/CLK     CLK ADJ FR 41.2 TO 20.6 MSEC/DAY



                              APPENDIX B
                  OUT-OF-LIMITS & ALERTS OCCURRENCES
                      Week ending 24 October 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 24 October 2003

                     CLOCK DRIFT RATE ADJUSTMENTS

ORBIT          TIME                   CLOCK RATE CHANGE
-----          -----                  -----------------
66203          291/0220               CLK ADJ FR 0.0 TO 20.6 MSEC/DAY
66261          294/2239               CLK ADJ FR 20.6 TO 41.2 MSEC/DAY
66288          296/1834               CLK ADJ FR 41.2 TO 20.6 MSEC/DAY


                              APPENDIX D
                     UARS BATTERY PERFORMANCE DATA
                      Week ending 24 October 2003

     17 October 2003 - GMT Day 290 Beta = 57.4 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    -700.0/-700.0 -3.05/-4.62  +00.0/+00.0  07.2     0.000     0.0
2     +11.2/-22.4  +4.51/+2.60  +22.4/-14.4  26.4     1.030    17.1
3     +16.8/-22.4  +3.23/+1.97  +22.0/-14.4  26.4     1.020    16.7


     24 October 2003 - GMT Day 297 Beta = 67.3 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    -700.0/-700.0 -2.74/-4.31  +00.0/+00.0  07.2     0.000     0.0
2     +11.2/-22.4  +3.55/+1.97  +19.2/-15.2  26.7     1.050    15.7
3     +11.2/-33.6  +2.60/+1.34  +18.8/-14.8  26.7     1.050    15.4

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


                              APPENDIX E
                         UARS ANOMALY REPORTS
                      Week ending 24 October 2003

                     NEW ANOMALY REPORTS GENERATED
AR NO.    SUBSYS    ORBIT     TIME      CDS       PROBLEM/DATA LOSS
------    ------    -----     ----      ---       -----------------
03-050    FOT       66301     297/1406  30832     Generic Late Acquisition

                 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
------    ------    -----     ----      ---       -----------------
03-050    FOT       See List  Oct 03    30832     Generic Late Acquisition