An edition of Aerodynamic test and analysis of a turbojet-boosted launch vehicle concept (spacejet) over a Mach number range of 1.50 to 2.86 (1981)

Aerodynamic test and analysis of a turbojet-boosted launch vehicle concept (spacejet) over a Mach number range of 1.50 to 2.86

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Aerodynamic test and analysis of a turbojet-b ...
Gregory D Riebe, Gregory D Rie ...
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Last edited by Open Library Bot
December 3, 2010 | History
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An edition of Aerodynamic test and analysis of a turbojet-boosted launch vehicle concept (spacejet) over a Mach number range of 1.50 to 2.86 (1981)

Aerodynamic test and analysis of a turbojet-boosted launch vehicle concept (spacejet) over a Mach number range of 1.50 to 2.86

by

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Publish Date
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service]
Language
English
Pages
52

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Subjects

Aerodynamics, Supersonic, Supersonic Aerodynamics, Winged spacecraft

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Cover of: Aerodynamic test and analysis of a turbojet-boosted launch vehicle concept (spacejet) over a Mach number range of 1.50 to 2.86
Aerodynamic test and analysis of a turbojet-boosted launch vehicle concept (spacejet) over a Mach number range of 1.50 to 2.86
1981, National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service]
in English
  • Not in Library

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Book Details

Edition Notes

"Langley Research Center."

Subject category 02

"July 1981"--Cover

Includes bibliographical references

Published in
Washington, D.C, [Springfield, Va
Series
NASA technical paper -- 1888

The Physical Object

Pagination
52 p. :
Number of pages
52

ID Numbers

Open Library
OL14932972M

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Download catalog record: RDF / JSON
December 3, 2010 Edited by Open Library Bot Added subjects from MARC records.
January 20, 2010 Edited by WorkBot add subjects and covers
December 11, 2009 Created by WorkBot add works page