UARS Weekly Status Report

15 August 2003




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                UARS WEEKLY STATUS REPORT - 15 August 2003

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

During this week, SOLSTICE continued to operate in good health gathering
solar data on all available orbital tracking periods. We gathered 
collaborative data with Tuesday's successful TIMED/SEE calibration 
rocket (NASA 36.205). This week we received about 55% of each day's data 
amounting to about 550 minutes of solar observing time per day.

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

SUSIM successfully gathered all of its daily mid 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.

***********
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 2002129 has been 
reprocessed and archived at the GSFC DAAC.  HEPSA data files from 2002130
through 2002149 are processed and awaiting archiving at the DAAC.

     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.

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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.

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

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

                           REPORTING PERIOD

This  report covers 02 August 2003 (Orbit 65044, GMT Day 214)  through
08 August 2003 (Orbit 65149, GMT Day 220).


                         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           215/1207      65066     POWER ON - DAY ONLY
       PEM           216/1532      65084     POWER ON (BEGIN)
       HRDI          217/2040      65102     FULL-TIME TO DAY ONLY
       PEM           219/2214      65133     POWER OFF AXIS-1


The  beta  angle  ranged between the angles of 25.6  degrees  to  39.5
degrees  for  this  report period.  The beta angle is  now  increasing
towards a maximum angle of 42 degrees on 11 August 2003 (DOY 223).

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 01 August and 08  August
2003 are provided in Appendix D.

The  clock  error  ranged from -06.8 to 04.9 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       =    00
    PEM       =    03
    HRDI      =    01


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

    FOT  =    05

Five (5) Anomaly Reports remained OPEN at the end of this report period
(see Appendix E).


                        GROUND SYSTEM OPERATION

Five  (5) 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 suggestion to go to the VT-6 charge level one day prior to the yaw
maneuver was approved at the UARS Monthly Status Meeting.  This was
suggested in order to keep the differential voltage down prior to the
yaw.  This change will be implemented for the reverse to forward yaw
maneuver on 26 August 2003.



                               MEETINGS


The  FOT  attended  the  UARS Monthly Status  Review  to  present  the
significant events from the month of July.

The  FOT  also attended the biweekly UARS DRB meeting to  review  open
Eclipse DRs.




                       FUTURE SIGNIFICANT EVENTS

The  next  UARS  Yaw slew is scheduled for 27 August 2003  (DOY  239).
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 08 August 2003

ORBIT   AOS        NO.      SUBSYS      REASON
-----   ---        ---      ------      ------
65066   215/1207   03-202   PEM         POWER ON - DAY ONLY
65081   216/1205   03-203   PEM AXIS-1  POWER ON ATTEMPTS
65084   216/1532   03-203   PEM AXIS-1  POWER ON (BEGIN)
65084   216/1532   03-203   PEM AXIS-1  POWER ON (CONCLUSION)
65102   217/2040   03-204   HRDI        FULL-TIME TO DAY ONLY
65133   219/2214   03-205   PEM         POWER OFF AXIS-1



                              APPENDIX B
                  OUT-OF-LIMITS & ALERTS OCCURRENCES
                      Week ending 08 August 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 08 August 2003

                     CLOCK DRIFT RATE ADJUSTMENTS

ORBIT          TIME                   CLOCK RATE CHANGE
-----          -----                  -----------------
-None this report period.



                              APPENDIX D


                     UARS BATTERY PERFORMANCE DATA
                      Week ending 08 August 2003

     01 August 2003 - GMT Day 213 Beta = 22.5 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  07.2     0.000     0.0
2     +00.0/-123.2 +6.44/+4.83  +28.8/-15.2  24.3     1.030    20.9
3     +22.4/-50.4  +5.15/+3.87  +28.0/-15.2  24.2     1.020    20.6


     08 August 2003 - GMT Day 220 Beta = 39.5 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/-50.0  07.2     0.000      0.0
2     +11.2/-123.2 +5.47/+4.19   +26.4/-50.0  25.0     1.030     20.0
3     +22.4/-67.2  +4.51/+3.23   +25.6/-50.0  25.0     1.030     20.0

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


                              APPENDIX E
                         UARS ANOMALY REPORTS
                      Week ending 08 August 2003

                     NEW ANOMALY REPORTS GENERATED
AR NO.    SUBSYS   ORBIT    TIME      CDS      PROBLEM/DATA LOSS
------    ------   -----    ----      ---      -----------------
03-037    FOT      65059    215/0007  30832    Generic Late Acquisition
03-038    FOT      65061    215/0304  33390    Degraded data
03-039    FOT      65081    216/1205  N/A      PEM AXIS-1 Power ON Problem
03-040    FOT      65099    217/1634  33399    Dropouts / COP status changes
03-041    FOT      65120    219/0110  33410    Negative Acquisition 1KB Omni

                 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
------    ------   -----     ----      ---      -----------------
03-037    FOT      See List  August 03 30832    Generic Late Acquisition
03-038    FOT      65061     215/0304  33390    Degraded data
03-039    FOT      65081     216/1205  N/A      PEM AXIS-1 Power ON Problem
03-040    FOT      65099     217/1634  33399    Dropouts / COP status changes
03-041    FOT      65120     219/0110  33410    Negative Acquisition 1KB Omni