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Summary of solid rocket motor plume flow field and radiation analysesThe inclusion of solid propellant plume flow field effects in analyses and design of the space vehicle was investigated. Results of these analyses are summarized.
Document ID
19800015868
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Audeh, B. J. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Carter, R. E. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Smith, S. D. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
September 4, 2013
Publication Date
April 1, 1980
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-161456
LMSC-HREC-TR-D697900
Report Number: NASA-CR-161456
Report Number: LMSC-HREC-TR-D697900
Accession Number
80N24361
Funding Number(s)
CONTRACT_GRANT: NAS8-28609
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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