Validation of high aspect ratio cooling in a 89 kN (20,000 lb[sub f]) thrust combustion chamber

Validation of high aspect ratio cooling in a ...
Mary F. Wadel
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Last edited by WorkBot
January 20, 2010 | History

Validation of high aspect ratio cooling in a 89 kN (20,000 lb[sub f]) thrust combustion chamber

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Cover of: Validation of high aspect ratio cooling in a 89 kN (20,000 lb[sub f]) thrust combustion chamber
Validation of high aspect ratio cooling in a 89 kN (20,000 lb[sub f]) thrust combustion chamber
1996, National Aeronautics and Space Administration, National Technical Information Service, distributor
Microform in English

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Book Details


Edition Notes

Shipping list no.: 98-0769-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.

Published in
[Washington, DC], [Springfield, Va
Series
NASA technical memorandum -- 107270.

The Physical Object

Format
Microform
Pagination
1 v.

ID Numbers

Open Library
OL15496512M

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January 20, 2010 Edited by WorkBot add subjects and covers
December 11, 2009 Created by WorkBot add works page