Intermetallic and ceramic matrix composites for 815 to 1370 C (1500 to 2500 F) gas turbine engine applications

Intermetallic and ceramic matrix composites f ...
Joseph R. Stephens, Joseph R. ...
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Last edited by Open Library Bot
December 3, 2010 | History

Intermetallic and ceramic matrix composites for 815 to 1370 C (1500 to 2500 F) gas turbine engine applications

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Cover of: Intermetallic and ceramic matrix composites for 815 to 1370 C (1500 to 2500 F) gas turbine engine applications
Intermetallic and ceramic matrix composites for 815 to 1370 C (1500 to 2500 F) gas turbine engine applications
1989, National Aeronautics and Space Administration, For sale by the National Technical Information Service
Microform in English

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Book Details


Edition Notes

Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1989. 1 microfiche.

Published in
[Washington, DC], [Springfield, Va
Series
NASA-TM -- 102326, NASA technical memorandum -- 102326..

The Physical Object

Format
Microform
Pagination
1 v.

ID Numbers

Open Library
OL17101123M

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December 3, 2010 Edited by Open Library Bot Added subjects from MARC records.
December 10, 2009 Created by WorkBot add works page