Item Details

Aeropropulsive Characteristics of Canted Twin Pitch-Vectoring Nozzles at Mach 0.20 to 1.20

Francis J. Capone, Mary L. Mason, and George T. Carson, Jr.
Format
Book; Government Document; Online; EBook
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1991.
Language
English
Series
NASA Technical Paper
Description
254 p. : ill. ; 28 cm.
Mode of access: Internet.
Notes
  • Prepared at Langley Research Center.
  • Chiefly statistical tables.
  • Bibliography: p. 13.
Series Statement
NASA technical paper ; 3060
Logo for Copyright Not EvaluatedCopyright Not Evaluated
Technical Details

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    a| Aeropropulsive characteristics of canted twin pitch-vectoring nozzles at Mach 0.20 to 1.20 / c| Francis J. Capone, Mary L. Mason, and George T. Carson, Jr.
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    a| Carson, George T.
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    a| Stability of airplanes.
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    a| Airplanes x| Control systems.
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    a| Airplanes x| Motors x| Thrust.
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