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Analysis of the trajectory, loads and heating experienced by a body passing through a supersonic flow fieldAnalytical methods for determination of trajectories, loads, and heating experienced by spacecraft passing through rocket exhaust field
Document ID
19670022023
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Butler, H. W. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Prozan, R. J. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
August 3, 2013
Publication Date
March 1, 1967
Subject Category
Thermodynamics And Combustion
Report/Patent Number
LMSC/HREC-A784084
HREC-1567-1
NASA-CR-84855
Report Number: LMSC/HREC-A784084
Report Number: HREC-1567-1
Report Number: NASA-CR-84855
Accession Number
67N31352
Funding Number(s)
CONTRACT_GRANT: NAS7-100
CONTRACT_GRANT: JPL-951567
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROCKET EXHAUST
HEAT EFFECT
AERODYNAMIC LOAD
TRAJECTORY ANALYSIS

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