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Space vehicle engine and heat shield environment review. Volume 1: Engineering analysisMethods for predicting the base heating characteristics of a multiple rocket engine installation are discussed. The environmental data is applied to the design of adequate protection system for the engine components. The methods for predicting the base region thermal environment are categorized as: (1) scale model testing, (2) extrapolation of previous and related flight test results, and (3) semiempirical analytical techniques.
Document ID
19740021099
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mcanelly, W. B. (Teledyne Brown Engineering Huntsville, AL, United States)
Young, C. T. K. (Teledyne Brown Engineering Huntsville, AL, United States)
Date Acquired
September 3, 2013
Publication Date
December 1, 1973
Subject Category
Propulsion Systems
Report/Patent Number
EE-MSFC-1774
NASA-CR-120243
Report Number: EE-MSFC-1774
Report Number: NASA-CR-120243
Accession Number
74N29212
Funding Number(s)
CONTRACT_GRANT: NAS8-27802
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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