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Aug 1975

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1975esabu.......26h&link_type=abstract

ESA Bulletin, Aug. 1975, p. 26-30.

Mathematics

Probability

Cos-B Satellite, Instrument Packages, Spaceborne Telescopes, Spacecraft Design, X Ray Telescopes, Attitude Indicators, Data Systems, Reliability Engineering, Satellite Attitude Control, Spacecraft Launching, Support Systems

Scientific paper

The schematic diagram, block diagram, and functional elements of the cylindrical spin-stabilized COS-B satellite are discussed. The basic design principle was to keep all supporting subsystems as simple as possible, both to reduce the development time and costs and to meet the design reliability requirement of 85% probability of mission success for a planned one-year lifetime.

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