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Analytical methods for computing the effects of turbine exhaust and film-coolant injection on rocket engine performance

Author: Hosack, G A.
Published: [Place of publication not identified] : [publisher not identified], 1969.
Physical Description: 38 pages
Additional Creators: American Institute of Aeronautics and Astronautics. Technical Information Service

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Language Note

In English.

Subject(s)

Aeronautics

Collection

IAA papers.

Note

A69-32726.
Abstracted in International Aerospace Abstracts.

Reproduction Note

Microform. New York : American Institute of Aeronautics and Astronautics, Technical Information Service, [19--?]

View MARC record | catkey: 19137342