Along with initial program, analysis must be made of entire vehicle design requirements to establish components and environments; reliability goals and allocations of subsystem goals; to illustrate technique for estimating reliability, preliminary estimate for proposed spacecraft power supply subsystem is presented; reliability emphasis in design study using statistical methods to devise economical configuration of redundant design; design review method; reliability during development; subsystem qualification testing.
Reliable spacecraft designs
SAE -- Paper
SAE Meeting ; 1961 Design
1961
8 pages
Aufsatz (Konferenz)
Englisch
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