This International Standard defines the principles used to determine loads and the induced environment during the service life of a space flight vehicle and its components, taking account of the notions of probability, combined loads, corresponding safety factors and lifecycle. This title may contain less than 24 pages of technical content.
[PDF.oj84] Leman ISO 14622:2000, Space systems -- Structural design -- Loads and induced environment Rating: 3.65 (553 Votes)
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