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See handout -- annex 3
- M-CDR conclusion: need to understand spacecraft/experiment/operations
interactions. Study by Culhane taskforce.
- EM tests near successful completion
- Flight model: system schedule margins nearly depleted. Problems
with mass, power, and pointing budgets.
See handout -- annex 4
- Spacecraft: EM program to be completed on Feb. 10, 1994
- Attitude and orbital control: third gyro being implemented
- Power: subsystem to be delivered middle Feb. '94
- Launcher: First Atlas IIAS (AC 108) successfully launched
- Pointing: concerns about 4 reaction wheel, UVCS imbalance,
inter experiment jitter. Need to establish time lining for experiments.
Input request: Info for update S/C payload thermal model and load
analysis
See handout -- annex 5
- Organization: Heinrich Schröter appointed SOHO AIV engineer.
Helmut Schweitzer will focus on ground Ops together with Sergio Vaghi
- Power-thermal problem: optical properties of OSR too wide.
Solutions reviewed, PI's asked to endorse EID-A updated temperature
limits
- LASCO, UVCS, SUMER, and EIT must deliver
structural model updates at ESTEC by Feb. 7, '94
- Updated FM thermal models requested at ESTEC by Feb. 15, '94
- Scientific data recorded during EMC test to be picked up
and assessed by experimenters. ESA requires status report by
Feb. 7, '94. Experimenters desire visibility of their data during test.
Project will forward request to Matra
- FM programme: delivery schedule now critical, PI's must adhere
to schedule henceforth. ESA recommends that core team be put together
now, to fullfil FM PLM and S/C system test obligations
- Two options presented for SWT request that instrument EGSE's not
be put in cleanroom at KSC
See handout -- annex 6
Next: Status of Experiments
Up: Minutes of the
Previous: Agreed Agenda and
Bernhard Fleck
Tue Jan 6 15:25:37 EST 1998