Static aerodynamic characteristics of a single-stage-to-orbit vehicle with low planform loading at Mach numbers from 0.3 to 4.63

Static aerodynamic characteristics of a singl ...
Delma C. Freeman, Delma C. Fre ...
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Last edited by WorkBot
January 20, 2010 | History

Static aerodynamic characteristics of a single-stage-to-orbit vehicle with low planform loading at Mach numbers from 0.3 to 4.63

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Cover of: Static aerodynamic characteristics of a single-stage-to-orbit vehicle with low planform loading at Mach numbers from 0.3 to 4.63
Static aerodynamic characteristics of a single-stage-to-orbit vehicle with low planform loading at Mach numbers from 0.3 to 4.63
1977, National Aeronautics and Space Administration, Scientific and Technical Information Office, for sale by the National Information Service
in English
Cover of: Static aerodynamic characteristics of a single-stage-to-orbit vehicle with low planform loading at Mach numbers from 0.3 to 4.63
Static aerodynamic characteristics of a single-stage-to-orbit vehicle with low planform loading at Mach numbers from 0.3 to 4.63
1977, National Aeronautics and Space Administration, Scientific and Technical Information Office, for sale by the National Information Service
in English

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Book Details


Edition Notes

Issued Nov. 1977.

Includes bibliographical references.

Published in
[Washington], Springfield, Va
Series
NASA technical memorandum ; 74056, NASA technical memorandum -- 74056.

The Physical Object

Pagination
66 p. :
Number of pages
66

ID Numbers

Open Library
OL17647279M

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