An edition of Optimal pitch thrust-vector angle and benefits for all flight regimes (2000)

Optimal pitch thrust-vector angle and benefits for all flight regimes

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Optimal pitch thrust-vector angle and benefit ...
Glenn B. Gilyard, Glenn B. Gil ...
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Last edited by WorkBot
December 15, 2009 | History
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An edition of Optimal pitch thrust-vector angle and benefits for all flight regimes (2000)

Optimal pitch thrust-vector angle and benefits for all flight regimes

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Publish Date
Publisher
National Aeronautics and Space Administration, Dryden Flight Research Center, National Technical Information Service, distributor
Language
English
Pages
22

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Subjects

Airplanes, Angles (Geometry), Automatic flight control, Control surfaces, Drag (Aerodynamics), Flight testing, Handling characteristics, Lift (Aerodynamics), Motors, Pitch (Inclination), Thrust, Thrust vector control
Edition Availability
Cover of: Optimal pitch thrust-vector angle and benefits for all flight regimes
Optimal pitch thrust-vector angle and benefits for all flight regimes
2000, National Aeronautics and Space Administration, Dryden Flight Research Center, National Technical Information Service, distributor
Microform in English
Cover of: Optimal pitch thrust-vector angle and benefits for all flight regimes
Optimal pitch thrust-vector angle and benefits for all flight regimes
2000, National Aeronautics and Space Administration, Dryden Flight Research Center, National Technical Information Service, distributor
in English
Cover of: Optimal pitch thrust-vector angle and benefits for all flight regimes
Optimal pitch thrust-vector angle and benefits for all flight regimes
2000, National Aeronautics and Space Administration, Dryden Flight Research Center, National Technical Information Service, distributor
Microform in English
Cover of: Optimal pitch thrust-vector angle and benefits for all flight regimes
Optimal pitch thrust-vector angle and benefits for all flight regimes
2000, National Aeronautics and Space Administration, Dryden Flight Research Center, National Technical Information Service, distributor
Microform in English
Cover of: Optimal pitch thrust-vector angle and benefits for all flight regimes
Optimal pitch thrust-vector angle and benefits for all flight regimes
2000, National Aeronautics and Space Administration, Dryden Flight Research Center, National Technical Information Service, distributor
Microform in English
Cover of: Optimal pitch thrust-vector angle and benefits for all flight regimes
Optimal pitch thrust-vector angle and benefits for all flight regimes
2000, National Aeronautics and Space Administration, Dryden Flight Research Center, National Technical Information Service, distributor
Microform in English

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Book Details

Edition Notes

"March 2000."

"Performing organization report number H-2402"--Report documentation page.

Includes bibliographical references.

Performed by NASA Dryden Flight Research Center for National Aeronautics and Space Administration WU 522-16-14-00-39-00-LIO

Published in
Edwards, Calif, [Springfield, Va
Series
NASA/TM -- 2000-209021, NASA technical memorandum -- 2000-209021.

The Physical Object

Pagination
22 p. :
Number of pages
22

ID Numbers

Open Library
OL20639635M

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History

Download catalog record: RDF / JSON / OPDS | Wikipedia citation
December 15, 2009 Edited by WorkBot link works
October 29, 2008 Created by ImportBot Imported from University of Toronto MARC record