R. W. Michel

Combustion performance and heat transfer characterization of LOX/hydrocarbon type propellants

final report, volume 1

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Author

R. W. Michel

Contributions

United States. National Aeronautics and Space Administration. - Contributor

Publication

1983 - Aerojet Liquid Rocket Company, Sacramento, Calif, California

Language

English

Word Count

0 words, Guess

Page Count

0 pages

Physical Format

Microform

Identifiers

Open LibraryOL16117594M

Subjects

Topics

Liquid oxygen Space shuttles Cryogenic rocket propellantsOxygen-hydrocarbon rocket engines

Series Statement

[NASA contractor report] -- CR-171713.
NASA contractor report -- NASA CR-171713.

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