UARS Weekly Status Report

03 March 2000




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                UARS WEEKLY STATUS REPORT - 03 Mar 2000

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

We continue to gather enough data to meet all the SOLSTICE science
objectives during this period of reduced tape recorder operations. 
SOLSTICE operates normally, collecting solar data on all available 
orbital tracking periods and stellar calibration observations whenever 
possible.

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

SUSIM continues to gather a near normal set of daily solar scans that
are scheduled for periods of predicted telemetry.

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

Nothing received.

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

     The PEM spectrometers continue to be active under PMON control*.  AXIS-2
was activated on February 29 to complete the total AXIS activation.  At the 
present time, PEM energy deposition is not being generated.  Recent data 
configuration changes have affected PEM software causing multiple failures.  
These failures are being reviewed by the PEM team.  In order to correct for new 
telemetry requirements, PEM will most likely need to update processing code 
with a patch delivery.  At this time, updated HEPS calibration parameters will 
be submitted.  These will influence the in-situ energy deposition predictions, 
so new versions of PEM energy deposition Level 3 files will be generated.

 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
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Nothing received.

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

Nothing received.

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

The following report from WINDII was received on 25 Feb, 
but it was accidently overlooked when the 25 Feb 2000 
Status Report was prepared.


WINDII REPORT FOR THE WEEK ENDING February 25, 2000

WINDII is next scheduled to operate March 5-16, 2000. 

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

Routine processing of instrument Daily Activity Plans continues  
with no problems.  The instrument operations schedule for the
next yaw period (21 March to 25 April 2000) was coordinated 
and distributed.

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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.
        *2 days ATT (7.3)   PROD                 (2R-2C=0L)
        *2 days OBC (3.4)   PROD                 (2R-2C=0L)
        *1 day  PEM (3.32)  PROD (L1-L2)         (1R-1C=0L)
        *2 days SUS (7.2)   PROD (L1-L3)         (2R-2C=0L)
        18 days WIN (5.11A) PROD (L1-L3)         (522R-482C-14F=40L)
         2 days SEN (5.0)   PROD (1992)          (2R-2C=0L)

*The CDHF reprocessed ATTITUDE, OBC, PEM, and SUSIM against the LEVEL0
 data that was re-ingested with better quality for UARS DAY 3083 and 3084.
  
Data created in the month of December 1999 has been loaded into the DAAC
Transfer Tables for HALOE, NMC, UKMO, and PEM.

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

                                    REPORTING PERIOD

This report covers 19 February, 2000 (Orbit 46129, GMT Day 050) through 25 
February 2000 (Orbit 46233, GMT Day 056).


                                 SPACECRAFT OPERATION

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

                           INSTRUMENT OPERATIONAL CHANGES

               Instrument     Time        Orbit      Comment
               PEM            055/0008    46203      AXIS-1 On

The beta angle ranged between the angles of 9.4 degrees to 35.2 degrees for 
this report period.  The beta angle is now increasing toward a maximum angle 
of 51 degrees on 04 March 1999 (DOY 064).

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 0.7 to 1.0 degrees C.  
Additional battery performance data for each battery on 18 February 2000 and 25 
February 2000 are provided in Appendix D.

The clock error ranged from 10.7 to -10.8 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   =  02
%     ALERTS          =  00

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

%     FOT             =  015
%     HALOE           =  02
%     PEM             =  01

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

%     FOT             =  01

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

TRANSPONDER FREQUENCIES:
7 Transponder A:  00/021  -  2287.496849
7 Transponder B:  00/031  -  2287.498836


                              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 00/055 show the observatory data loss to be 565 hours, 38 
minutes, 19.273 seconds (an increase of 0 minutes 0 seconds since the last report 
period).

100 percent data capture was observed this past week.


                             OTHER SIGNIFICANT EVENTS

                              UARS SATELLITE OPERATIONS

The FOT worked on SCS-21 by providing data for the development of a new trending 
system for UARS.  The FOT has been providing instruction into the details on the 
capabilities of the current trending utility.  The FOT is looking forward to an 
improvement in this area.  A new trending tool could reduce trend time from hours to 
minutes.  In addition, the FOT also provided to the SCS-21 folks, a list and snaps 
of all display pages.

                                  MEETINGS

February 24, 2000 (DOY 055) - The FOT went over to the Landsat 5 operations control 
center to observe their inclination maneuver.  That mission is similar to the UARS 
mission therefore it was interesting to relate the configuration and dynamics of the 
maneuvers to the UARS spacecraft


                        FUTURE SIGNIFICANT EVENTS

The next UARS Yaw slew is scheduled for March 21, 2000 (DOY 081).  This maneuver 
will be a Forward to Reverse Flight maneuver (Northern Hemisphere viewing).

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 February 2000

    ORBIT     AOS         NO.        SUBSYS    REASON
    -----     ---         ---        ------    -------
    46129    050/0055     00-057     HALOE     Power ON
    46133    050/0755     00-058     HALOE     HTR MTR ON
    46140    050/1848     00-059     NBTR      NBTR MANAGEMENT
    46147    051/0616     00-059     NBTR      NBTR MANAGEMENT
    46155    051/1817     00-060     NBTR      NBTR MANAGEMENT
    46161    052/0435     00-060     NBTR      NBTR MANAGEMENT
    46170    052/1857     00-061     NBTR      NBTR MANAGEMENT
    46176    053/0439     00-061     NBTR      NBTR MANAGEMENT
    46191    054/0442     00-062     NBTR      NBTR MANAGEMENT
    46199    054/1644     00-062     NBTR      NBTR MANAGEMENT
    46200    054/1905     00-063     NBTR      NBTR MANAGEMENT
    46203    055/0008     00-064     PEM       PEM AXIS 1 ON
    46211    055/1313     00-066     OBC       Clk Adj fr 0.00 to 20.6 msec/day
    46214    055/1647     00-063     NBTR      NBTR MANAGEMENT
    46215    055/1828     00-065     NBTR      NBTR MANAGEMENT
    46221    056/0448     00-065     NBTR      NBTR NOOPS
    46230    056/1911     00-067     NBTR      NBTR NOOPS
    46233    056/2333     00-068     OBC       Clk Adj fr 20.6 to 0.00 msec/day

____________________________________________________________________________________

                                     APPENDIX B
                         OUT-OF-LIMITS & ALERTS OCCURRENCES
                            Week ending 25 February 2000

The following Out-Of-Limits occurrences were detected:

     MNEMONIC        STATE     DESCRIPTION                 ORBITS
     ---------       -----     ------------                ------
     PEAXTHERM6Z     Y-HI      PEM AXIS THERM 6Z TEMP      46211-18
     HRPTSPBIMON     Y-HI      HRDI PB MONITOR             46211,15-18

The following ALERT occurrences were detected:

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

____________________________________________________________________________________

                                     APPENDIX C
                        CLOCK & SOLAR ARRAY RATE CORRECTIONS
                            Week ending 25 February 2000

                             CLOCK DRIFT RATE ADJUSTMENTS

     ORBIT           TIME                     CLOCK RATE CHANGE
     -----           ----                     -----------------
     46211         055/13:13 (24 Feb 00)      from 0.00 to 20.6 msec/day
     46233         056/23:33 (25 Feb 00)      from 20.6 to 0.00 msec/day

_________________________________________________________________________________

                                    APPENDIX D
                          UARS BATTERY PERFORMANCE DATA
                          Week ending 25 February 2000

     18 Feb 2000 - GMT Day 049 Beta = 9.4 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    -67.2/-89.6   -3.68/-4.94  +0.0/+0.0     16.0      0.000     0.0
2    +33.6/-22.4   +5.15/+3.87  +30.4/-13.6   25.1      1.030     20.2
3    +134.4/11.2   +3.87/+2.60  +29.6/-15.2   25.0      1.027     19.6

     25 Feb 2000 - GMT Day 056 Beta = 35.2 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    -56.0/-89.6   -3.05/-4.31  +0.0/+0.0     16.0      0.000     0.0
2    +89.6/-5.6    +5.79/+4.83  +29.2/-15.2   25.1      1.028     22.5
3    +89.6/+0.0    +5.15/+3.87  +28.8/-16.4   25.1      1.026     22.2

                              V/T LEVEL CHANGES
ORB#                  TIME                     LVL FR-TO
-----                 ----------               ----------
                      no changes               V/T 5
____________________________________________________________________________________
 
                                    APPENDIX E
                              UARS ANOMALY REPORTS
                          Week ending 25 February 2000

                          NEW ANOMALY REPORTS GENERATED
AR NO.     SUBSYS     ORBIT     TIME     TTR     PROBLEM/DATA LOSS
------     ------     -----     ----     ---     -----------------
00-004     FOT        46142   050/2136   14170   Generic Late Acquisition

                      ANOMALY CLOSURE INFORMATION RECEIVED
AR NO.     SUBSYS     ORBIT     TIME     TTR     PROBLEM/DATA LOSS
------     ------     -----     ----     ---     -----------------
                           No new reports generated

                      ANOMALY INVESTIGATION REPORTS GENERATED
AR NO.     SUBSYS     ORBIT     TIME     TTR     PROBLEM/DATA LOSS
------     ------     -----     ----     ---     -----------------
                           No new reports generated

                              OPEN ANOMALY REPORTS
AR NO.     SUBSYS     ORBIT     TIME     TTR     PROBLEM/DATA LOSS
------     ------     -----     ----     ---     -----------------
99-064     FOT     44135     10/8-9/99   N/A     HRDI Cal Lamp Errors
99-071     FOT     44398     299/1212    21512   TPF Not Receiv 512 PB
00-004     FOT     see list  Feb 00      14170   Generic Late Acq.
	 	SEVNTFW00/08