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Application of the MESA reactive hydrocode to space vehicle explosive ordnance devicesThe construction of detailed computational models of the dynamic behavior of various explosive ordnance devices used on space vehicles is discussed. The following topics are presented in viewgraph form: numerical methods, explosives and detonations, and the MESA computer code.
Document ID
19930010961
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Goldstein, Selma (Aerospace Corp. Los Angeles, CA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1993
Publication Information
Publication: NASA. Stennis Space Center, The First NASA Aerospace Pyrotechnic Systems Workshop
Subject Category
Propellants And Fuels
Accession Number
93N20150
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19930010943Collected WorksThe First NASA Aerospace Pyrotechnic Systems Workshop
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