UARS Weekly Status Report

26 FEBRUARY 1999




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                UARS WEEKLY STATUS REPORT - 26 FEB 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
***********

SUSIM successfully gathered its normal solar, offset, and occultation
data without apparent problems.

Reprocessing of the SUSIM data to data version 20 continues.

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

     PEM is active under PMON control.  Energy processor #6 for the 
HEPS-1 unit has been found to not activate correctly.  Data affected 
are from the upper energy EE channel for Head-2 of HEPS-1 (that is the 
+15 deg electrons above 300 keV).  Tests are being conducted on this 
energy processor to assure that it is operating correctly.  Measurements 
from this sensor will be activated as soon as possible.  The PEM team 
and FOT are convinced that the entanglement of energy processor #6
is related to OBC control and not a failure of that energy processor.
Early attempts at adjusting OBC command timing have not been successful.
The FOT is attempting to refine their diagnostics and confine the 
problem.

     While under PMON control, the PEM instrument computes energy deposition
from the HEPS unit.

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

HALOE was turned on February 23, 1999.  All engineering parameters are nominal.

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

The instrument is now off as scheduled. MLS is scheduled to begin south viewing
operations on Feb 27 and operate though Mar 4. 

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

HRDI continues to operate normally.
Recently, a significant recalibration of the HRDI interferometers was
performed.  The HRDI Fabry-Perot etalons have been slowly drifting out of
parallelism since the beginning of the mission and this has led to a slow
decrease in the instrument sensitivity.  On December 31, 1998, the HRDI
instrument performed a calibration to allow this drift to be corrected.
These calibration data were used to calculate new coefficients for the
instrument computer.  On January 29, 1999 the new coefficients were entered
into the instrument processor and have been used by the instrument since.
As expected, the signal levels for all observed features rose to levels
comparable to those that were observed at the beginning of the mission.  A
consequence of this change of coefficients is that the "zero wind" value
for the instrument is now different and currently unknown which introduces
a bias into the wind.  We are in the process of evaluating the new zero,
but until that is completed the HRDI data products from January 29 onward
should not be used.  We will notify the community when the data is again
valid.

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

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. 

***********
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.
           6 days ATT (7.3)  RSS  (Y2K Version)(6R-6C=0L)
           0 days HAL (4.80) PROD (L3)         (1874R-1721C-1F=152L)
           2 days HAL (4.81) PROD (TEST L1-L3) (2R-2C=0L)
          46 days PEM (3.32) PROD (OA-L2)      (760R-130C=630L)
          67 days SUS (7.0)  PROD              (647R-67C=580L)
               
The CDHF re-ingested level 0 for UARS day 2710 (julian 99/042)
due to better data quality.  This ingest was completed on 02/18/99.

The CDHF is scheduling the upgrade of Multinet to V4.1b as part of the ongoing 
Y2K implementation effort.

CDHF pending software upgrades:  DEC AXP Fortran 6.5, DEC AXP OPEN
VMS 6.2, OpenIngres
 
DAAC data created in the month of December 1998 has been loaded into the
DAAC Transfer Tables for HALOE, HRDI, NMC, PEM, and UKMO.
                  
***********
FOT
***********

This report covers 13 February 1999 (Orbit 40571, GMT Day 044 through 19 
February 1999

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
         HALOE      048/2241   40645     Off
         PEM        049/0017   40646     Cal test

The beta angle ranged between the angles of 34.1 degrees to 6.1 degrees for 
this report period.  The beta angle is now decreasing toward a minimum 
angle of -2 degrees for the next yaw on 20 February 1999 (DOY 051).

The annular solar eclipse that occurred on 16 February 1999 over the Indian 
Ocean, Australia and the South Pacific Ocean had little to no effect on 
UARS power.

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 1.3 degrees C.  Additional battery performance data 
for each battery on 12 February 1999 and 19 February 1999 are provided in 
Appendix D.

The clock error ranged from 9.9 to -11.8 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 =     02

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

%     FOT     02
%     HALOE   01
%     PEM     03

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

%     FOT     05

Six (6) Anomaly Report remained OPEN at the end of this report period (see 
Appendix E).

TRANSPONDER FREQUENCIES:
          Transponder A:  99/019  -  2287.496951
          Transponder B:  99/020  -  2287.499045


GROUND SYSTEM OPERATION

Two (2) operational support problems occurred this period.  Anomaly Reports 
are included in Appendix E.

Week Ending 12 February 1999

The data loss calculations supplied by Data Capture Facility (DCF) from 
mission start through UTC Day 99/042 show the observatory data loss to be 
22 hours, 46 minutes, 16.564 seconds (an increase of 55 minutes and 25.024

seconds since last report period).  This is a 0.0351 percent data loss 
which equals a 99.9649 percent data capture for the mission.

The increase of 55 minutes and 25.024 seconds occurred over two (2) days:

7 10.112 seconds on Day 036 due to data hit and insufficient overlap, and
7 55 minutes and 14.912 seconds on day 042 due to power outage 
complications.

Week Ending 19 February 1999

The data loss calculations supplied by Data Capture Facility (DCF) from 
mission start through UTC Day 99/049 show the observatory data loss to be 
22 hours, 46 minutes, 25.972 seconds (an increase of 09.408 seconds since 
last report period).  This is a 0.0351 percent data loss which equals a 
99.9649 percent data capture for the mission.

The increase of 09.408 seconds occurred over three (3) days:

7 0.512 seconds on Day 043 due to data hit,
7 8.384 seconds on Day 044 due to power outage complications, and
7 0.512 seconds on Day 047 due to data hit.

NCC switched their operational scheduling database to the "NCC-98" database 
release on 12 February.  Due to some minor problems with the migration of 
"previously scheduled" TDRS contacts from the old database to the NCC-98 
database, most POCCs were required to delete and re-add all of their 
scheduled TDRS contacts spanning days 044-059.  If the POCCs failed to 
delete and re-add those events, the ability to send successful GCMRs during 
the events in this time period would not exist.  Due to the important need 
for sending GCMRs, the UARS FOT deleted and re-added all of their 
previously scheduled events during the day 044-059 time period.

The FOT received and processed the remaining Y2K "test" 8-week planning 
aids that were requested by SOLSTICE operations (via the MPG).  Two of the 
seven planning aids were invalid and need to be regenerated by FDF.  The 
other five planning aids were copied to a special account on the UMPGAL 
system, where they will be made available to all interested instrument 
operations teams.

The UARS Test and Training Simulator (UTTS) remains non-operational.  The 
estimated time to repair the UTTS and return it to operation is unknown.


OTHER SIGNIFICANT EVENTS

UARS SATELLITE OPERATIONS

The FOT continues to support the PEM team with diagnosis of the Energy 
Processor 6 status error.  FOT attempted two tests, one a manual activation 
of the instrument, and the other a redesign of the timing of PEM commands 
for day-only.  The first test established that EP6 can be commanded on by 
the real-time activation sequence.  The second test did not bring up EP6.  
The FOT created another activation plan using real-time command sequences 
to emulate the PMON activation sequence.

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

Planning continues for the simulator testing.


UARS RE-ENGINEERING - TELEMETRY PROCESSING - No change



MEETINGS

FOT supported a meeting with Booz-Allen & Hamilton representatives (David 
Taylor) on 18 February to discuss the daily operations timeline for UARS.



FUTURE SIGNIFICANT EVENTS

The next UARS Yaw Around Maneuver is scheduled for 20 February 1999.


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 19 February 1999

ORBIT      AOS      NO.     SUBSYS         REASON
-----      ---      ---     ------         -------  
40572   044/0142   99-066   OBC         Clk Adj fr 0.00 to 20.6 msec/day
40595   045/1444   99-067   OBC         Clk Adj fr 20.6 to 0.00 msec/day
40614   046/2052   99-068   PEM         HEPS Command
40645   048/2241   99-069   HALOE       Power OFF
40646   049/0017   99-070   PEM         Calibration/testing
40662   050/0158   99-071   PEM         Calibration/testing

_______________________________________________________________

                               APPENDIX B
                  OUT-OF-LIMITS & ALERTS OCCURRENCES
                      Week ending 19 February 1999

MNEMONIC           STATE      DESCRIPTION                    ORBITS
---------          -----      ------------                   ------
NBRECBI             Y-HI    NBTR B Current                 40612
NBRECBI             Y-HI    NBTR B Current                 40627


The following ALERT occurrences were detected:

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

_______________________________________________________________

                              APPENDIX C
                 CLOCK & SOLAR ARRAY RATE CORRECTIONS
                       Week ending 19 February 1999

                      CLOCK DRIFT RATE ADJUSTMENTS

     ORBIT              TIME                 CLOCK RATE CHANGE
     -----              ----                 -----------------
     40572     044/01:50 (12 Feb 99)     from 0.00 to 20.6 msec/day
     40595     045/14:48 (14 Feb 99)     from 20.6 to 0.00 msec/day

_______________________________________________________________


                             APPENDIX D
                    UARS BATTERY PERFORMANCE DATA
                       Week ending 19 February 1999


     12 Feb 1999 - GMT Day 043 Beta = 34.1 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     0.0/-11.   -3.05/-4.31   +0.0/ +0.0    16.8    0.000    0.0
2   +56.0/ 0.0   +5.47/+4.51  +30.4/-14.4    26.2    1.030   21.1
3   +56.0/-11.2  +4.51/+3.55  +29.6/-14.4    26.1    1.027   20.8


     19 Feb 1999 - GMT Day 050 Beta = 6.1 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    0.0/-22.4   -3.68/-4.94   +0.0/ +0.0    16.8    0.000    0.0
2  +67.2/ 0.0    +4.83/+3.87  +31.2/-14.4    25.6    1.016   20.8
3  +89.6/-5.6    +3.87/+2.60  +30.4/-14.4    25.4    1.017   20.4


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



                               APPENDIX E
                         UARS ANOMALY REPORTS
                      Week ending 19 February 1999


                       NEW ANOMALY REPORTS GENERATED
 AR NO.  SUBSYS    ORBIT      TIME      TTR      PROBLEM/DATA LOSS
 ------  ------    -----      ----      ---      -----------------
99-007    FOT      40577    044/1019    N/A      no lock on 32k OBC dump
99-008    FOT      40589    045/0419    20585    "No UARS RF, no TDEtrk"
99-009    FOT      40590    045/0650    14170   Generic Late Acquisition
99-010    FOT      40591    045/0838    N/A     6 masked ATC Dump errors
99-010    FOT      40636    048/0750    N/A     GCMR to 32k on Q invalid


                 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
  ------   ------       -----      ----       ---      -----------------
99-006      FOT        see list     Feb 99     14170     Generic Late Acq



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