An edition of Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m℗ø(350 psia)
(1987)
Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m℗ø(350 psia)
by Tamara A. Smith
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Publish Date
1987
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Office,
For sale by the National Technical Information Service]
Language
English
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Subjects
Nozzles, Rockets (Aeronautics), Rocket enginesShowing 1 featured edition. View all 1 editions?
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1
Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m℗ø(350 psia)
1987, National Aeronautics and Space Administration, Scientific and Technical Information Office, 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], 1987. 1 microfiche.
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| January 19, 2010 | Edited by WorkBot | add subjects and covers |
| December 11, 2009 | Created by WorkBot | add works page |