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Power System Performance of the SOHO Spacecraft During the 1998 Attitude Recovery
Technical Paper
1999-01-2484
ISSN: 0148-7191, e-ISSN: 2688-3627
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English
Abstract
This paper will highlight the electrical power system topology and basic performance of the SOHO mission during the first two years of its operation. It will go on to relate the chronology of spacecraft and power system events that occurred from the initial loss of SOHO contact in June 1998, up until the time of its attitude recovery some three months later. It will describe the operational modes of the power system during this critical period and the fundamental lessons learnt, which could enhance recovery prospects in the event that other missions experience a similar anomaly.
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Citation
Fiebrich, H., Haines, J., Perol, P., and Rumle, P., "Power System Performance of the SOHO Spacecraft During the 1998 Attitude Recovery," SAE Technical Paper 1999-01-2484, 1999, https://doi.org/10.4271/1999-01-2484.Also In
References
- The SOHO Recovery WebPage http://sohowww.nascom.nasa.gov/operations/ Recovery/
- The SOHO Mission Interruption Joint NASA/ESA Investigation Board
- SOHO Recovery Jean-Phillipe Olive, MMS (at NASA Goddard) Flight Mechanics Conference
- SOHO Power Subsystem Architecture and Design P. Rumler, ESA/ESTEC, Noordwijk, The Netherlands. M. Assie, MMS, Toulouse, France. E. Mourembles, MMS, Toulouse, France. A. Polli, FIAR, Milan, Italy 1993 European Space Power Conference, Graz, Austria