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1/4: P50 Wiring

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Title: 1/4: P50 Wiring


1
1/4 P50 Wiring Materials
Science Working Group April 20th, 2008
STEREO Project
Ron Denissen APL Project Manager Andy Driesman
APL Mission System Engineer
2
STEREO Phase E Organization Chart
Project Scientist M. Kaiser
Mission Director S. Odendahl Mission System
Engineer J. La
Project Manager R. A. Denissen
Science Teams
SSC W. Thompson
Payload Operations Teams
Mission Operations D. Ossing
System Engineering A. Driesman
DSN Technical
Mission Operation Team
Subsystem Lead Engineers
GSFC
APL
FDF
DSN Scheduling
JPL
NRL, UCBerkeley, UNH, UMinn
3
Program Assessment
Resources
Technical
Schedule
Programmatic
Jan Feb Mar
Jan Feb Mar
Jan Feb Mar
Jan Feb Mar
G
G
G
Y
Y
G
G
G
G
G
G
G
G
G
Detailed Description (for items identified
as yellow or red)
  • Technical
  • Both Observatories operational. And collecting
    prime science data
  • ST Anomaly investigation complete. Report due
    out shortly. Mitigation in place.
  • Schedule
  • Routine operations HGA and instrument cals,
    momentum dumps.
  • Resources
  • No staffing or funding concerns at this time.
  • Programmatic
  • No issues at this time.

Major problem Identified solution Commitment is
in jeopardy
Major problem No identified solution Commitment
cannot be met
No current problem All commitments can be met
Y
R
G
4
Program Status
  • Mission Operations
  • Operations team reduced 7
  • MOC is manned 5 days a week, 8 hours a day
  • 1 attended track per week on each observatory
    (more if requested)
  • Mission operations center collecting, on average,
    7 Gbits per day in support of the prime science
    mission.
  • Special Observatory Events
  • 44 instrument calibration events
  • 14 High Gain Antenna Calibrations
  • 20 Momentum Dumps (every 6 weeks on ahead, 8
    weeks on behind)
  • Software Patches and Parameter adjustments to RAM
  • Autonomy Rule Changes in RAM and EEPROM

5
Program Summary
  • Transitioned to Phase E January 22nd , 2007
  • The observatories are in operational mode and
    about 47 degrees apart.
  • No planned GC or CDH flight software loads.
  • Spacecraft A operating on IMU2 due to failure of
    the X-gyro in IMU1
  • Star Tracker anomaly occurred late December 2007.
  • Data rate decrease about August 2008.
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