UARS Weekly Status Report

30 APR 1999




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                UARS WEEKLY STATUS REPORT - 30 APRIL 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.

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

After turning back on April 11th, SUSIM gathered its normal solar,
offset, and occultation data without apparent problems.

Reprocessing of the SUSIM data to version 20 is now complete through
UARS day 2523.

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

     PEM is active under PMON control.  Energy processor #6 for the HEPS-1 unit 
is activating correctly now.  The PEM team and FOT found that the entanglement 
of energy processor #6 was related to the differences between OBC activation 
commanding and activation commanding from the ground.  Attempts at adjusting OBC
command timing failed until the correct combination of command sequence was 
found.  The FOT and the PEM team are completing close-out documentation on this
problem.

     While under PMON control, the PEM instrument computes energy deposition
from the particle spectrometers.

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

HALOE was operating successfully prior to its scheduled turn off on April
27, 1999.  All engineering parameters were nominal and the science data
results are of excellent quality.

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

Nothing received.

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

Nothing received.

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

WINDII successfully completed its observation period of April 25-29.
Reprocessing and the evaluation of reprocessed data are continuing. 

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

Y2K end-to-end test successfully completed Thursday April 29, 1999.

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.
         1 day  CLA (7.0)  PROD (TEST) (L1-L3)  (1R-1C=0L)
        50 days PEM (3.32) PROD (OA-L2)         (760R-578C-1F=181L)
         1 day  SOL (4.62) TEST (DEBUG)(L2-L3)  (1R-1F=0L)
       111 days WIN (5.11) PROD (LOG)           (2014R-1303C=711L)
        76 days WIN (5.11) PROD (L1-L3)         (2014R-339-3F=1672L).

DAAC data created for February 1999 has been loaded into the DAAC transfer
tables. DAAC data thru January 1999 for HALOE, HRDI, PEM, NMC, and UKMO is
revealed/available to the User community. The CDHF will load March 1999
current day DAAC data in May 1999.

SOLSTICE "The debug SOLSTICE job was resubmitted with debug changes, and again
aborted due to "general unrecoverable error", this time reported by 
ASGCAL.  Investigation of this error will take place next week."

CDHF pending software upgrades:  DEC AXP Fortran 6.5, DEC AXP OPEN
VMS 6.2, OpenIngres.
                  
***********
FOT
***********

This report covers 17 April 1999 (Orbit 41515, GMT Day 107 through 
23 April GMT Day 113).


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
                 HRDI       107/0037     41515     Day Only
                 PEM        107/0040     41515     AXIS On
                WINDII      109/2307     41559     Off
                 PEM        109/2307     41559     AXIS-2 Off
                 HRDI       113/0059     41605     Full Time

The beta angle ranged between the angles of 46.5 degrees to 30.0 degrees 
for this report period.  The beta angle is now decreasing toward a minimum 
angle of 2.9 degrees on 30 April 1999 (DOY 120).

Two manually generated Stellar offset maneuvers were performed on GMT days 
111 and 112 at the request of SOLSTICE operations.  The offsets are similar 
to the normal weekly SOLSTICE offset which usually occurs during a Solar 
tracking session.

A series of SSPP gridded offset maneuvers were performed on GMT days 107 
through 112 at the request of SUSIM operations.  The offsets utilized the 5 
and 10 arc-minute interval steps, as opposed to the optional 15 and 30 arc-
minute intervals.

A UARS TDRS event was scheduled partially out of view on GMT day 112 due to 
FOT error.  This event was not one of UARS' originally scheduled events, 
but was added in real time to replace an event that NCC had taken away for 
a higher priority TDRS user.  While scheduling the new event, the FOT 
mistakenly used only the TDRS view periods contained on the UPS graphical 
display, instead of the CMS generated HG Antenna Tracking report.  Due to 
slewing limitations, the view periods on HG tracking report are often more 
restrictive than the view periods on the UPS, because the UPS does not take 
into account the physical operation of the HG antenna.  In this particular 
case, the High Gain Antenna began to slew to the other TDRS approximately 3 
minutes into the newly scheduled event, resulting in a tape recorder 
playback data loss.  An Anomaly Investigation Report (AIR 99-022) is being 
written to document this problem.

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 16 April 1999 and 23 April 1999 are provided in 
Appendix D.

The clock error ranged from -11.1 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.

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

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

%     FOT     03
%     HRDI    01
%     PEM     02
%     WINDII  01


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

%     FOT     05

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

TRANSPONDER FREQUENCIES:
          Transponder A:  99/054  -  2287.496923
          Transponder B:  99/055  -  2287.498750


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) was not 
available this week.

The FOT is still awaiting the delivery of the 8-week Ground Track Y2K test 
file from FDF.  This file was expected to be delivered this week, but was 
not received as of the end of this reporting period.


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.

A first cut of the high level UARS mission support requirements for the 
IMOC were completed on Friday.  These requirements were presented and 
discussed in a Friday Meeting with Evan Eller.

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 - No change


UARS PROPULSION MODULE B/D THRUSTER LINE FILL - No change


MEETINGS

FOT supported the weekly IMOC meeting on 21 April 1999.


FUTURE SIGNIFICANT EVENTS

The next UARS Yaw Around Maneuver (reverse-to-forward) is scheduled for 30 
April 1999 (DOY 120).


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 23 April 1999

ORBIT       AOS       NO.    SUBSYS          REASON
-----       ---       ---    ------          -------  
41515    107/0040   99-140   PEM AXIS   Power ON
41517    107/0402   99-141   OBC        Clk Adj fr 20.6 to 0.00 msec/day
41547    109/0404   99-142   OBC        Clk Adj fr 0.00 to 20.6 msec/day
41559    109/2307   99-143   WINDII     Power ON
41559    109/2307   99-144   AXIS2      Power OFF
41570    110/1701   99-145   HRDI       PMON Exercise
41575    111/0059   99-146   OBC        Clk Adj fr 20.6 to 0.00 msec/day

_______________________________________________________________

                               APPENDIX B
                  OUT-OF-LIMITS & ALERTS OCCURRENCES
                      Week ending 23 April 1999

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 23 April 1999

                      CLOCK DRIFT RATE ADJUSTMENTS

     ORBIT              TIME                 CLOCK RATE CHANGE
     -----              ----                 -----------------
     41517     107/04:04 (17 Apr 99)     from 20.6 to 00.0 msec/day
     41547     109/04:10 (19 Apr 99)     from 00.0 to 20.6 msec/day
     41575     111/01:02 (21 Apr 99)     from 20.6 to 00.0 msec/day


_______________________________________________________________


                             APPENDIX D
                    UARS BATTERY PERFORMANCE DATA
                       Week ending 23 April 1999


     16 Apr 1999 - GMT Day 106 Beta = 46.5 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   -56.0/-78.4   -3.05/-4.31  +0.0/ +0.0    16.6    0.000    0.0
2   +78.4/-5.6    +6.44/+4.51 +27.2/-16.0    24.3    1.019   22.1
3   +33.6/-33.6   +5.15/+3.87 +27.2/-16.8    24.2    1.023   21.8


     23 Apr 1999 - GMT Day 113 Beta = 30.0 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  -3.05/-4.31   +0.0/ +0.0    16.6    0.000    0.0
2   +56.0/-5.6   +6.11/+4.51  +30.4/-15.2    24.8    1.021   22.0
3   +44.8/-11.2  +5.15/+3.23  +29.6/-15.6    24.8    1.024   21.7


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



                               APPENDIX E
                         UARS ANOMALY REPORTS
                      Week ending 23 April 1999


                     NEW ANOMALY REPORTS GENERATED
   AR NO.  SUBSYS   ORBIT      TIME       TTR      PROBLEM/DATA LOSS
   ------  ------   -----      ----       ---      -----------------
99-019      FOT     41573     110/2154     20772   NASCOM PDP Failure
99-020      HRDI    41560     110/0051     N/A     HRDI 
99-016      FOT     41588     111/2157     14170   Generic Late Acquisition
99-021      HRDI    41589     112/0058     N/A     HRDI IN PMON MODE
99-022      FOT     41603     112/2149     N/A     Data Loss


                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
  ------  ------   -----      ----       ---      -----------------
99-016      FOT     see list  Apr 99      14170   Generic Late Acq
99-019      FOT     41573     110/2154    20772   NASCOM PDP Failure
99-020      HRDI    41560     110/0051    N/A     HRDI 
99-021      HRDI    41589     112/0058    N/A     HRDI IN PMON MODE
99-022      FOT     41603     112/2149    N/A     Data Loss

	 	SEVNTFW99/17