NASA NTRS · 19730022110
Statistical determination of space shuttle component dynamic magnification factors
Abstract
A method is presented of obtaining vibration design loads for components and brackets. Dynamic Magnification Factors from applicable Saturn/Apollo qualification, reliability, and vibroacoustic tests have been statistically formulated into design nomographs. These design nomographs have been developed for different component and bracket types, mounted on backup structure or rigidly mounted and excited by sinusoidal or random inputs. Typical nomographs are shown.
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Lehner, F.. 1973-05-31. Statistical determination of space shuttle component dynamic magnification factors. https://ntrs.nasa.gov/citations/19730022110
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