UARS Weekly Status Report

11 April 2003




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                UARS WEEKLY STATUS REPORT - 11 April 2003

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

This week, SOLSTICE was powered only during daylight for three days to
support the yaw maneuver. Otherwise, solar data were collected on all
available orbital tracking periods.

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

Nothing received.

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

Nothing received.

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

     The PEM web site has moved.  It has a new URL.  Access the PEM web site
using http://wwwpem.space.swri.edu.  The PEM data from the GUVI conjunction
periods has moved to http://wwwpem.space.swri.edu/guvi-pem.html.

     Level 2 PEM HEPSA data files are being reprocessed for submission to the 
DAAC.  This data has been designated as version 2; however, there is no format
difference from the version 1 data format.  Version 2 HEPSA data is being 
generated because it was discovered that there exists processing errors within
some of the HEPSA version 1 data files.  Thus, if you are using any HEPSA
version 1 data files from the DAAC, please replace them with the version 2
data files.  Currently, HEPSA data between 1991274 and 2001365 has been 
reprocessed and archived at the GSFC DAAC.  SwRI is working on reprocessing
data PEM for 2002.

     PEM continues to work with the GUVI team on the diagnosis of data from
the first conjunction period.  Analysis of the two conjunction passes showed
that the aurora as detected by GUVI was at higher latitude than UARS.  
GUVI images from other times from the first conjunction period show spatial
regions that both GUVI and PEM sampled when aurora was present.  Separation
is several minutes to 10's of minutes when both instruments saw aurora. 
PEM has seen no aurora during the second conjunction period.  Due to a 
spacecraft anomaly, no PEM data was collected during the third conjunction 
period.

     PEM continues to receive NMC data files from NOAA.  No problems have
been encountered.  NOAA has changed the binary structure of the NMC data and
PEM is now receiving two data streams, one in the original VAX format and the
other from their new binary format.



*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.

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

                           REPORTING PERIOD

This report covers 29 March 2003 (Orbit 63150, GMT Day 088) through 04
April 2003 (Orbit 63247, GMT Day 094).


                         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
       PEM AXIS      090/0046      63180     POWER OFF
       WINDII        091/0223      63196     POWER OFF
       PEM           092/2151      63223     POWER OFF
       HALOE         092/2334      63224     POWER OFF


The  beta  angle  ranged between the angles of 37.0  degrees  to  12.9
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 1.27 to 1.28 degrees C.  Additional
battery  performance data for each battery on 28 March  and  04  April
2003 are provided in Appendix D.

The  clock  error  ranged from -9.9 to 10.4 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         =    00

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

    FOT       =    02
    PEM       =    02
    WINDII    =    01
    HALOE     =    01



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

    FOT  =    01

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


                        GROUND SYSTEM OPERATION

One  (1)  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 received results of the investigation at White Sands regarding
the 085/0554-0623 UTC event.  Their investigation showed that the UARS
negative acquisition was do to a WSGT software problem.  Their
software was apparently showing receipt of the GCMRs sent by the FOT,
but in reality it was not receiving them.  This problem will be fixed
in the next software delivery scheduled for mid May to early June.  In
the meantime, the FOT is aware of this problem and can respond
accordingly should the anomaly reoccur.


                               MEETINGS


The  FOT  attended the UAR Monthly Status review to report  status  of
significant events for the month of March.

The  FOT also attended the weekly UARS DRB to review the open DRs  and
discuss the details of the next Eclipse software delivery


                       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 04 April 2003


ORBIT   AOS        NO.      SUBSYS      REASON
-----   ---        ---      ------      ------
63180   090/0046   03-077   AXIS        POWER OFF
63196   091/0223   03-078   WINDII      POWER OFF
63223   092/2151   03-079   PEM         POWER OFF
63224   092/2334   03-080   HALOE       POWER OFF
63230   093/0803   03-081   OBC/CLK     CLK ADJ FR 0.0 TO -20.6 MSEC/DAY
63248   094/1317   03-082   OBC/CLK     CLK ADJ FR -20.6 TO 0.0 MSEC/DAY



                              APPENDIX B
                  OUT-OF-LIMITS & ALERTS OCCURRENCES
                       Week ending 04 April 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 04 April 2003

                     CLOCK DRIFT RATE ADJUSTMENTS

ORBIT          TIME                   CLOCK RATE CHANGE
-----          -----                  -----------------
63230          093/0803               CLK ADJ FR 0.0 TO -20.6 MSEC/DAY
63248          094/1317               CLK ADJ FR -20.6 TO 0.0 MSEC/DAY







                              APPENDIX D
                     UARS BATTERY PERFORMANCE DATA
                       Week ending 04 April 2003

     28 March 2003 - GMT Day 087 Beta = 40.6 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  -173.6/-201.6  -3.05/-4.31  +00.0/+00.0  08.3     0.000     0.0
2   +11.2/-112.0  +6.11/+4.83  +27.6/-15.6  24.2     1.030    21.1
3   +22.4/-67.2   +5.15/+3.87  +27.2/-15.6  24.0     1.020    20.9


     04 April 2003 - GMT Day 094 Beta = 12.9 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  -179.2/-201.6  -3.68/-4.94  +00.0/+00.0  08.3     0.000     0.0
2   +11.2/-22.4   +4.51/+3.87  +26.8/-15.2  26.1     1.020    20.0
3   +22.4/-22.4   +3.23/+2.60  +25.6/-14.4  26.1     1.010    19.6


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



                              APPENDIX E
                         UARS ANOMALY REPORTS
                       Week ending 04 April 2003

                     NEW ANOMALY REPORTS GENERATED
AR NO.    SUBSYS    ORBIT     TIME      CDS       PROBLEM/DATA LOSS
------    ------    -----     ----      ---       -----------------
03-011    FOT       63226     093/0216  30832     Generic Late Acquisition

                 ANOMALY CLOSURE INFORMATION RECEIVED
AR NO.    SUBSYS    ORBIT     TIME      CDS       PROBLEM/DATA LOSS
------    ------    -----     ----      ---       -----------------
03-011    FOT       63226     093/0216  30832     Generic Late Acquisition
03-010    FOT       63108     085/0554  32514     No Acquisition (29
minutes)

                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
03-009    FOT       63069     082/1624  N/A       Invalid COP Status
03-011    FOT       63226     093/0216  30832     Generic Late Acquisition