UARS Weekly Status Report

08 OCTOBER 1999




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                UARS WEEKLY STATUS REPORT - 08 OCT 1999

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

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

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

Nothing received.

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

Nothing received.

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PEM
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Nothing receieved.

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HALOE 
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Nothing received.

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MLS
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Nothing received.

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HRDI
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Nothing received.

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WINDII
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Nothing received.

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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. 

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CDHF
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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.
        13 days CLA (7.0)   PROD (L1-L3)         (473R-299C-16F=158L)
         0 days GPI (4.05)  PROD (CLAES L3B)     (191R-164C-2F=25L)
        21 days SUSIM (7.1) PROD (L1-L2)         (56R-21C=35L)

The CDHF plans on testing HALOE V4.82 formal delivery software, and then the
WINDII delivery on the current CDHF.
  
Current day data created and cataloged in July 1999 has been loaded into the
DAAC Transfer Tables for HALOE, PEM, NMC, and UKMO.
      
UARS CDHF REHOST:      
The CDHF continues to integrate the "UARS" environment on CDHFA/B.
We are installing PI software - HALOE 4.82 new delivery - for testing.
FDF was contacted to establish a process to test dataflows to the rehosted
CDHF. 

CDHF pending software upgrades: none 
                  
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FOT
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REPORTING PERIOD

This report covers 25 September, 1999 (Orbit 43927, GMT Day 268) through 1 
October 1999 (Orbit 44030, GMT Day 274).


SPACECRAFT OPERATION

The observatory is now in Foward Flight (Southern Hemisphere viewing) and is 
performing nominally under two-battery operations.  The instrument operational 
changes were:

                       INSTRUMENT OPERATIONAL CHANGES

           Instrument     Time       Orbit     Comment
             HALOE      270/2122     43969     On

The beta angle ranged between the angles of 1.2 degrees to 25.7 degrees for 
this report period.  The beta angle is now increasing toward a maximum angle of 
50 degrees on 12 October 1999 (DOY 285).

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 1.0 to 1.3 degrees C.  Additional battery performance data for each 
battery on 24 September 1999 and 01 October 1999 are provided in Appendix D.

The clock error ranged from -9.9 to -2.1 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  =     05

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

%     HALOE   =     02

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

%     FOT     =     02

Zero (0) Anomaly Reports remained OPEN at the end of this report period (see 
Appendix E).


TRANSPONDER FREQUENCIES:
%     Transponder A:  99/242  -  2287.496953
%     Transponder B:  99/243  -  2287.499030


GROUND SYSTEM OPERATION

Two (2) operational support problems 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 99/273 show the observatory data loss to be 24 hours, 55 
minutes, 36.724 seconds (an increase of 10.656 seconds since the last report 
period).  This is a 0.0354 percent data loss which equals a 99.9646 percent 
data capture for the mission.

The increase of 10.656 seconds occurred over one (2) days:

7 2.080 seconds on Day 268 due to an Data hit.
7 8.576 seconds on Day 273 due to an Data hits, no overlap.


OTHER SIGNIFICANT EVENTS

UARS SATELLITE OPERATIONS

Began preparations for the Leonid shower in November.  More information about 
the shower and the impact to UARS orbit is being requested from FDF.  It is not 
expected to change much if at all.


YEAR 2000 OPERABILITY SUPPORT

We received all of the planning aids needed for all the time periods to be 
tested for Y2K.  The CMS processing will be completed on Monday and testing 
will be done on Tuesday and Thursday of next week.  Hopefully, in those two 
days we can complete everything that we need to verify mission success in the 
next millennium.


MEETINGS

The FOT attended a meeting at Goddard Corporate Park regarding the UARS Y2k 
status.  The primary focus was to evaluate what the obsticles were to complete 
Y2k certification and put the process back on schedule.  All in all the meeting 
was successful and testing will continue with the next product delivery from 
FDF.

FUTURE SIGNIFICANT EVENTS

A meeting to discuss the UARS Safehold configuration and concerns for the MPS 
and its batteries is planned for Wednesday, October 6.  This meeting will be a 
closed meeting with only the FOT and specialized engineering support attending.

PEM requested to have the timing in their turn on sequence tightened up in yet 
another area.  This is expected to be accomplished within the next few weeks.

The FOT plans on working with FDF to devise a plan to verify the integrity of 
the UAV files in an effort to prevent discrepancies between the FDF 3-day High 
Gain Gimbal Angles file (HGA), and the 4-week User Antenna View files (UAV).  A 
problem occured where TDRS view periods were incorrect following a UARS yaw 
maneuver.


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 1 October 1999

ORBIT        AOS         NO.      SUBSYS     REASON
-----        ---        ---       ------    -------
43969     270/2122     99-328     HALOE      Power ON
43972     271/0222     99-329     HALOE      Power ON, COMPLETED

________________________________________________________________


                            APPENDIX B
                 OUT-OF-LIMITS & ALERTS OCCURRENCES
                     Week ending 1 October 1999

The following Out-Of-Limits occurrences were detected:

MNEMONIC       STATE     DESCRIPTION                ORBITS
---------      -----     ------------               ------
HRPTSPBIMON     R-LO     HRDI PULSE BUS MONITOR     43969
PEMBIAS00E      R-HI     PEM BIAS                   43976
HRPTSPBIMON     Y-HI     HRDI PULSE BUS MONITOR     44005,6,8,14
HRPTSQBIMON     Y-HI     HRDI QUIET BUS MONITOR     44014
HRPTSPBIMON     Y-HI     HRDI PULSE BUS MONITOR     44018,20,21-3


The following ALERT occurrences were detected:

MNEMONIC                 DESCRIPTION               ORBITS
---------                ------------              ------
     No Alerts to report this report period.

_______________________________________________________________________________

                            APPENDIX C
                CLOCK & SOLAR ARRAY RATE CORRECTIONS
                    Week ending 1 October 1999

                     CLOCK DRIFT RATE ADJUSTMENTS

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


                            APPENDIX D
                    UARS BATTERY PERFORMANCE DATA
                     Week ending 1 October 1999

     24 Sept 1999 - GMT Day 267 Beta = 1.2 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   -112.0/-134.4  -3.05/-4.62   +0.0/+0.0   16.5   0.000    0.0
2    +33.6/-22.4   +5.47/+4.51  +29.6/-14.4  24.3   1.014   21.6
3    +33.6/-33.6   +4.51/+3.23  +28.8/-15.2  24.3   1.016   21.1


     DIFF V (mV)   TEMP (C)     CURR (amp)   EON V  AVE C/D  AVE
BAT  MAX/MIN       MAX/MIN      MAX/MIN      MIN    RATIO    DOD(%)
---  ----------    --------     ----------   -----  -------  ------
1   -112.0/-134.4  -2.73/-3.99   +0.0/+0.0   16.5    0.000   0.0
2    +16.8/-67.2   +6.44/+5.15  +30.4/-15.2  24.5    1.023  22.3
3    +22.4/-56.0   +5.47/+3.87  +30.0/-16.0  24.3    1.024  22.1


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



                        APPENDIX E
                   UARS ANOMALY REPORTS
                 Week ending 1 October 1999


                NEW ANOMALY REPORTS GENERATED
AR NO.     SUBSYS     ORBIT      TIME         TTR     PROBLEM/DATA LOSS
------     ------     -----      ----         ---     -----------------
99-061     FOT        43970     270/2216     21402    NEGATIVE ACQ.
99-058     FOT        43998     272/1917     14170    GENERIC LATE ACQ.


          ANOMALY CLOSURE INFORMATION RECEIVED
AR NO.     SUBSYS     ORBIT      TIME        TTR     PROBLEM/DATA LOSS
------     ------     -----      ----        ---     -----------------
99-058     FOT     see list     Sept 99     14170    Generic Late Acq.
99-059     FOT        43827     261/0856     N/A     TAC Crashed
99-060     FOT        43833     261/1906     N/A     TAC Crashed


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


                    OPEN ANOMALY REPORTS
AR NO.     SUBSYS     ORBIT     TIME     TTR     PROBLEM/DATA LOSS
------     ------     -----     ----     ---     -----------------
                 None this report period

	 	SEVNTFW99/40