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Rocket nozzle coolant channel thermal analysis program (E25107)A complete description of the liquid cooled rocket nozzle analysis program (E25107) is presented, including a users manual, program listing, and a sample problem. The program is recommended for use in designing liquid cooled rocket nozzles. In addition, it is adaptable to any system in which a liquid-cooled tubular structure is used to contain and direct the flow of a hot gas.
Document ID
19730017105
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Thompson, W. R. (Aerojet Nuclear Systems Co. Azusa, CA, United States)
Date Acquired
August 7, 2013
Publication Date
April 14, 1972
Subject Category
Propulsion Systems
Report/Patent Number
N8110R:72-036
NASA-CR-132185
Report Number: N8110R:72-036
Report Number: NASA-CR-132185
Accession Number
73N25832
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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