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Author Freeman, Delma C., author.

Title Comparison of Space Shuttle Orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests / Delma C. Freeman, Jr., and Barnard Spencer, Jr.

Publication Info. [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.

Copies

Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.60:1779    ---  Available
Description 1 online resource (33 pages) : illustrations.
text txt rdacontent
computer c rdamedia
online resource cr rdacarrier
Series NASA technical paper ; 1779
NASA technical paper ; 1779.
Note Title from title screen (viewed on Aug. 25, 2016).
"December 1980."
"Performing Organization: NASA Langley Research Center"--Report documentation page.
Bibliography Includes bibliographical references (page 8).
Type Of Report Technical paper.
Funding National Aeronautics and Space Administration 506-51-33-02 L-13945
Subject Artificial satellites -- Orbits.
Wind tunnels -- Ground simulators.
Space vehicles -- Landing.
Stability of space vehicles.
Artificial satellites -- Orbits. (OCoLC)fst00817381
Space vehicles -- Landing. (OCoLC)fst01128032
Stability of space vehicles. (OCoLC)fst01131228
Wind tunnels -- Ground simulators. (OCoLC)fst01175721
Ailerons.
Approach and landing tests (STS)
Elevons.
Lateral stability.
Longitudinal stability.
Space Shuttle Orbiters.
Genre/Form Online resources.
Electronic books.
Electronic government information.
Added Author Spencer, Bernard, 1932- author.
Langley Research Center, author.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.
Other Form: Print version: Freeman, Delma C. Comparison of space shuttle orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests (OCoLC)7330682
Microfiche version: Freeman, Delma C. Comparison of space shuttle orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests (OCoLC)711544700
Gpo Item No. 0830-H-15 (online)
Sudoc No. NAS 1.60:1779

 
    
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