UARS Weekly Status Report

14 January 2005




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                UARS WEEKLY STATUS REPORT - 14 JAN 2005

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

SOLSTICE began day only operations on January 11 in support of the yaw 
maneuver. Otherwise, the instrument continues to perform exceptionally, 
taking solar data on all available orbital tracking periods. An average 
of 59% of data were returned this week accounting for 420 minutes of 
solar observing time.

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

SUSIM was turned off for the yaw around on Jan. 10.  Before that,
the experiment successfully gathered daily mid (1.1 nm) resolution,
MgII, occultation, solar pointing offset, and continuous monitoring
scans for time periods with UARS telemetry or tape recording.

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

Nothing received.

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

Nothing received.

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

Nothing received.

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

Nothing received.

***********
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.
                  
***********
FOT
***********


                           REPORTING PERIOD

This  report covers 01 January 2005 (Orbit 72835, GMT Day 001) through
07 January 2005 (Orbit 72939, GMT Day 007).


                         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
       HALOE         001/1326      72843     POWER ON
       PEM           001/2335      72849     AXIS OFF
       PEM           006/2324      72924     ZEPS/NEPS DAY-ONLY TO OFF



The beta angle ranged between the angles of 48.0 degrees to 22.2
degrees for this report period.  The beta angle is now decreasing
towards a minimum angle of 2.0 degrees on 12 January 2005 (DOY 012).

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 0.97 to 1.28 degrees C.  Additional
battery performance data for each battery on 31 December 2004 and 07
January 2005 are provided in Appendix D.

The clock error ranged from 09.3 to -03.8 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       =    00
    HALOE     =    02
    PEM       =    02


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

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 continued their CMS software acceptance testing this week.
This testing will continue into the new year.  The goal for completion
is no later than end of January 2005.

                               MEETINGS


-None this report period.


                       FUTURE SIGNIFICANT EVENTS

The next UARS Yaw slew is scheduled for 12 January 2005 (DOY 012).
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 07 January 2005

ORBIT   AOS        NO.      SUBSYS      REASON
-----   ---        ---      ------      ------
72843   001/1326   05-001   HALOE       POWER ON PT 1
72844   001/1509   05-002   HALOE       POWER ON PT 2
72849   001/2335   05-003   PEM         AXIS OFF
72924   006/2324   05-004   PEM         ZEPS/NEPS DAY-ONLY TO OFF


                              APPENDIX B
                  OUT-OF-LIMITS & ALERTS OCCURRENCES
                      Week ending 07 January 2005

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 07 January 2005

                     CLOCK DRIFT RATE ADJUSTMENTS

ORBIT          TIME                   CLOCK RATE CHANGE
-----          -----                  -----------------
-NONE THIS REPORT PERIOD.

                              APPENDIX D
                     UARS BATTERY PERFORMANCE DATA
                      Week ending 07 January 2005

     31 December 2004 - GMT Day 366 Beta = 79.4 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 -3.68/-4.62  +00.0/+00.0  07.0     0.00      0.0
2      44.8/ -11.2 +4.51/+3.87  +23.2/-14.4  26.7     1.05     16.7
3     -11.2/ -89.6 +3.23/+2.60  +22.0/-13.6  26.7     1.04     16.1

     07 January 2005 - GMT Day 007 Beta = 22.2 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/-4.31  +00.0/+00.0  07.0     0.00      0.0
2      22.4/ -33.6 +6.44/+5.47  +29.6/-14.0  26.2     1.04     20.0
3     -11.2/-190.4 +5.15/+3.87  +28.0/-13.2  26.2     1.03     19.0


     V/T LEVEL CHANGES
ORB#           AOS TIME   LVL FR-TO
-----          --------   ---------
-NONE THIS REPORT PERIOD.


                              APPENDIX E
                         UARS ANOMALY REPORTS
                      Week ending 07 January 2005

                     NEW ANOMALY REPORTS GENERATED
AR NO.    SUBSYS    ORBIT     TIME      CDS       PROBLEM/DATA LOSS
------    ------    -----     ----      ---       -----------------
05-001    FOT       72843     001/1326  30832     Generic Late Acquisition

                 ANOMALY CLOSURE INFORMATION RECEIVED
AR NO.    SUBSYS    ORBIT     TIME      CDS       PROBLEM/DATA LOSS
------    ------    -----     ----      ---       -----------------
04-090    FOT       See List  Dec 04    30832     Generic Late Acquisition
04-094    FOT       72814     365/1550  30853     Late Acquisition

                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
------    ------    -----     ----      ---       -----------------
05-001    FOT       72843     001/1326  30832     Generic Late Acquisition