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Load relief autopilot analysis to minimize launch vehicle peak thrust vector deflection requirements / by Leslie L. Scalzott and Fred Teren.

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Format:
Book
Author/Creator:
Scalzott, Leslie L., author.
Teren, Fred, author.
Contributor:
United States. National Aeronautics and Space Administration, issuing body.
Series:
NASA technical note ; D-4786.
NASA technical note ; D-4786
Language:
English
Subjects (All):
Automatic pilot (Airplanes).
Physical Description:
1 online resource (ii, 39 pages) : illustrations.
Place of Publication:
Washington, D.C. : National Aeronautics and Space Administration, September 1968.
Notes:
Includes bibliographical references (page 39).
Description based on online resource; title from PDF title page (NASA, viewed Dec. 21, 2020).
Other Format:
Print version: Scalzott, Leslie L. Load relief autopilot analysis to minimize launch vehicle peak thrust vector deflection requirements
OCLC:
761196833

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