UARS Weekly Status Report

02 JULY 1999




********************************************************************

                UARS WEEKLY STATUS REPORT - 02 JUL 1999

********************************************************************

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

SOLSTICE continues to operate normally, collecting solar data on all 
available orbital tracking periods and stellar calibration observations, 
whenever possible.  

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

SUSIM was turned on as scheduled on June 30 after being off for 6 days.  
Completion of the turn-on procedure was delayed by telemetry problems at 
White Sands, resulting in the loss of solar data on June 30.  Normal 
operations, including the planned "monthly" calibration scans of 
deuterium lamp spectra, were resumed on July 1.

We are evaluating the recently reprocessed V20 products before their
release to the DAAC.

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

Nothing received.

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

     The PEM/AXIS activated on June 30.  While AXIS is active, it produces
energy deposition from 16 pixels based on precipitating electrons derived 
from measured X-ray fluxes.

     The PEM spectrometers continue to be active under PMON control.  While 
under PMON control, the PEM instrument computed energy deposition from its 
particle spectrometers.

     The FOT and the PEM team are completing close-out documentation on 
the HEPS Energy Processor trouble; however progress has been hampered 
with the departure of Peter Thomas.

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

HALOE continues successful operations with all engineering parameters
within nominal operating range.  HALOE science data products continue to be
of excellent quality.

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

Nothing received.

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

Nothing received.

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

Nothing received.

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

Routine processing of instrument Daily Activity Plans continues  
with no problems.  The MPG continues to assist the Project 
Scientist with the scheduling of instrument operations. 

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

The CDHF processed current day data through level 3 for all active
instruments. Additionally, CDHF personnel reprocessed: (R)= Requested
 (C) = Complete, (F)= Failed  (L) = Days remaining to reprocess.
        10 days CLA (7.0)  PROD (L1-L3)         (475R-71C-8F=396L)
         0 days GPI (4.05) PROD (MLS V5 3AL)    (39R-0C-1F=39L)
        50 days WIN (5.11) PROD (L1-L3)         (1540R-837C-5F=698L)


***********
FOT
***********

REPORTING PERIOD


This report covers 19 June 1999 (Orbit 42459 , GMT Day 170) through 25 June 
(GMT Day 176).

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
                ACRIM      173/2334     42518     Off
                SUSIM      173/2334     42518     Off
                 MLS       174/0129     42519     On

The beta angle ranged between the angles of 22.7 degrees to 33.5 degrees 
for this report period.  The beta angle is now increasing toward a maximum 
angle of 34 degrees on 26 June 1999 (DOY 177).

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 23.8 V end-of-night (EON) load bus voltage.  
Battery temperatures are stable with a temperature delta between Battery 2 
and Battery 3 of 0.9 to 1.1 degrees C.  Additional battery performance data 
for each battery on 18 June 1999 and 25 June 1999 are provided in Appendix 
D.

The clock error ranged from 9.9 to -10.5 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.

%     ALERTS         =  00
%     OUT-OF-LIMITS  =  04

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

%     MLS     08
%     FOT     02
%     ACRIM   01
%     SUSIM   01


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

%     FOT     01

No Anomaly Reports remained OPEN at the end of this report period (see 
Appendix E).

TRANSPONDER FREQUENCIES:
          Transponder A:  99/130  -  2287.496913
          Transponder B:  99/151  -  2287.499087


GROUND SYSTEM OPERATION

One (1) operational support problem occurred this period.  Anomaly Reports 
are included in Appendix E.

The data loss calculations supplied by Data Capture Facility (DCF) from 
mission start through UTC Day 99/119 show the observatory data loss to be 
24 hours, 13 minutes, 08.340 seconds (an increase of 0.000 seconds since 
the last report period).  This is a 0.0356 percent data loss which equals a 
99.9644 percent data capture for the mission.



OTHER SIGNIFICANT EVENTS

UARS SATELLITE OPERATIONS

FOT personnel are supporting the IMOC (SCS-21) development effort.  The 
current work is a continuation of the SCS-21 UARS implementation effort 
done last year which culminated in a level 1 demonstration.

The FOT continues to investigate the feasibility of a new PMON action to 
change battery V/T curves based on loading to mitigate battery risks in sun 
pointing safehold.

YEAR 2000 OPERABILITY SUPPORT

The end-to-end testing has been delayed until a new FORMATS software 
release can be made to accommodate the special Y2K planning aids.


MEETINGS

None


FUTURE SIGNIFICANT EVENTS

The next UARS Yaw Around Maneuver (reverse-to-forward) is scheduled for 10 
July 1999 (DOY 191).


PERSONNEL CHANGES

None



Attachments:  Appendix A,   Real-time Commands 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 25 June 1999

ORBIT        AOS        NO.     SUBSYS         REASON
-----        ---        ---     ------         -------  
42497     172/1355     99-207   OBC     Clk Adj 0.00 to 20.6 msec/day
42517     173/2149     99-208   OBC     Clk Adj 20.6 to 0.00 msec/day
42518     173/2334     99-209   ACRIM   Power OFF
42518     173/2334     99-210   SUSIM   Power OFF
42519     174/0129     99-211   MLS     Power ON
42522     174/0721     99-212   MLS     SCAN ACT OFF
42529     174/1700     99-213   MLS     SCAN ACT ON
42534     175/0136     99-214   MLS     MLS Stop/Run
42537     175/0710     99-215   MLS     MLS Stop/Run
42543     175/1556     99-216   MLS     MLS Stop/Run
42547     175/2231     99-217   MLS     SCAN ACT OFF
42548     176/0014     99-218   MLS     SCAN ACT ON/MPL Load

_______________________________________________________________

                              APPENDIX B
                  OUT-OF-LIMITS & ALERTS OCCURRENCES
                        Week ending 25 June 1999

MNEMONIC          STATE      DESCRIPTION         ORBITS
---------          -----      ------------       ------
HRPTSPBIMON       Y-HI     PTS P/B Cur Mon     42489-90,94
HRPSEQBIMON       Y-HI     HRDI Q/B Cur Mon    42521
MLSCANACTTMP      Y-LO     MLS Scan Act Temp   42522
MLSCANACTTMP      Y-LO     MLS Scan Act Temp   42541

The following ALERT occurrences were detected:

MNEMONIC                     DESCRIPTION          ORBITS
---------                   ------------          ------
     None this report period

_______________________________________________________________

                              APPENDIX C
                 CLOCK & SOLAR ARRAY RATE CORRECTIONS
                        Week ending 25 June 1999

                      CLOCK DRIFT RATE ADJUSTMENTS

     ORBIT            TIME                    CLOCK RATE CHANGE
     -----            ----                    -----------------
     42497     172/13:55 (21 June 99)     from 00.0 to 20.6 msec/day
     42517     173/21:56 (22 June 99)     from 20.6 to 00.0 msec/day



                              APPENDIX D
                    UARS BATTERY PERFORMANCE DATA
                        Week ending 25 June 1999


     18 June 1999 - GMT Day 169 Beta = 22.7 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   -95.2/-123.2 -2.73/-3.99   +0.0/ +0.0    16.5    0.000    0.0
2   +56.0/-5.6   +7.09/+5.15  +30.4/-15.2    23.8    1.021   22.7
3   +22.4/-50.4  +5.79/+4.19  +29.6/-16.0    23.7    1.024   22.5


     25 June 1999 - GMT Day 176 Beta = 33.5 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   -95.2/-123.2 -2.42/-3.68   +0.0/ +0.0    16.5    0.000    0.0
2   +22.4/-39.2  +6.44/+5.47  +29.2/-15.2    24.2    1.023   22.5
3   +22.4/-67.2  +5.47/+4.51  +28.8/-15.6    24.2    1.025   22.2


V/T LEVEL CHANGES
ORB#   TIME          LVL FR-TO
-----  --------      ----------
     no changes     V/T 5



                              APPENDIX E
                         UARS ANOMALY REPORTS
                        Week ending 25 June 1999


                     NEW ANOMALY REPORTS GENERATED
  AR NO.   SUBSYS    ORBIT      TIME       TTR      PROBLEM/DATA LOSS
  ------   ------    -----      ----       ---      -----------------
99-028     FOT       42493     172/0853   14170     Generic Late Acq.


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


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


                         OPEN ANOMALY REPORTS
  AR NO.   SUBSYS    ORBIT      TIME       TTR      PROBLEM/DATA LOSS
  ------   ------    -----      ----       ---      -----------------
99-028     FOT     see list   June 99     14170     Generic Late Acq.

	 	SEVNTFW99/26