Item Details

Wind-Tunnel Investigation at Supersonic Speeds of a Canard-Controlled Missile With Fixed and Free-Rolling Tail Fins

A.B. Blair, Jr., Langley Research Center
Format
Book; Government Document; Online; EBook
Published
[Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978.
Language
English
Series
NASA Technical Paper
SuDoc Number
NAS 1.60:1316
Description
76 p. : ill. ; 27 cm.
Mode of access: Internet.
Notes
  • Sept. 1978.
  • Includes bibliographical references.
Series Statement
NASA technical paper ; 1316
Logo for No Copyright - United StatesNo Copyright - United States
Technical Details

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    a| 76 p. : b| ill. ; c| 27 cm.
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    a| Aerodynamics, Supersonic.
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    a| Guided missiles x| Design and construction.
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