Purpose of paper is to provide estimate of effect of spacecraft vibration qualification test on vibration reliability of spacecraft system; vibration stress distribution, estimated from measurements and specification requirements, is formulated in terms of equipment qualification test level and combined with equipment strength distribution; vibration reliability of equipment is then related to that of space craft, and latter is formulated in terms of equipment qualification test level and number of equipments to be qualified; estimated reliability is given for range of vibration levels for which data were obtained.
Estimate of effect of spacecraft vibration qualification testing on reliability
U S Naval Research Laboratory -- Shock Vibration -- Bull
1967
18 pages
Aufsatz (Zeitschrift)
Englisch
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