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Pressure And Thermal Modeling Of Rocket LaunchesReport presents mathematical model for use in designing rocket-launching stand. Predicts pressure and thermal environment, as well as thermal responses of structures to impinging rocket-exhaust plumes. Enables relatively inexperienced analyst to determine time-varying distributions and absolute levels of pressure and heat loads on structures.
Document ID
19950070437
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Smith, Sheldon D. (SECA, Inc.)
Myruski, Brian L. (SECA, Inc.)
Farmer, Richard C. (SECA, Inc.)
Freeman, Jon A. (SECA, Inc.)
Date Acquired
August 16, 2013
Publication Date
November 1, 1995
Publication Information
Publication: NASA Tech Briefs
Volume: 19
Issue: 11
ISSN: 0145-319X
Subject Category
Physical Sciences
Report/Patent Number
MFS-26283
Accession Number
95B10616
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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