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Applications of variable property heat-transfer and friction equations to rocket nozzle coolant passages and comparison with nuclear rocket test results

Author
Taylor, M. F.
Published
[Place of publication not identified] : [publisher not identified], 1970.
Physical Description
10 pages
Additional Creators
American Institute of Aeronautics and Astronautics. Technical Information Service

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Language Note
In English.
Subject(s)
Collection
IAA papers.
Note
Abstracted in International Aerospace Abstracts.
A70-33622.
Reproduction Note
Microform. New York : American Institute of Aeronautics and Astronautics, Technical Information Service, [19--?]
View MARC record | catkey: 19144743