Abstract In general, the structural design of spacecraft structures, instruments, and structural elements is based on the static load factors specified in the launch vehicle (L/V) user’s guide(s) or by other quasi-static load (QSL) specifications. In this chapter, the calculated random load factors are based on the values of the interface loads of a particular system and depend on the random load levels, natural frequencies, and associated modal effective masses. If the random load factors are beyond the specified quasi-static load factors, adaptation (notching) of the random dynamic loads may be considered. Examples and problems with answers included are provided.
Random Vibration Load Factors
2018-01-01
12 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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