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A shock spectra and impedance method to determine a bound for spacecraft structural loadsA method to determine a bound of structural loads for a spacecraft mounted on a launch vehicle is developed. The method utilizes the interface shock spectra and the relative impedance of the spacecraft and launch vehicle. The method is developed for single-degree-of-freedom models and then generalized to multidegree-of-freedom models.
Document ID
19740027187
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bamford, R. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Trubert, M. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1974
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-140177
JPL-TM-33-694
Accession Number
74N35300
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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