Optimization For Whipple Shields Under Normal Impact

Details Optimization For Whipple Shields Under Normal Impact Optimization For Whipple Shields Under Normal Impact

Jan 2002

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2002iaf..confe.473l&link_type=abstract

IAF abstracts, 34th COSPAR Scientific Assembly, The Second World Space Congress, held 10-19 October, 2002 in Houston, TX, USA.,

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An engineering structural optimization methodology of Whipple Shields is developed designed to defeat hypervelocity impacts of meteoroids and space debris. The major unique of the optimization model presented in the paper is that Hypervelocity Impact Physical Model based on One-Dimension Impact Theory is incorporated into the previous optimization model. A space debris environment model is incorporated into an overall optimization methodology. And the determination of the initial optimization point and the geometric limitations of the design variables are added in the design process. The calculated results are compared with that of experimental optimization model.

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