Wind-tunnel investigation at supersonic speeds of a canard-controlled missile with fixed and free-rolling tail fins
By: A. B. Blair, Jr., Langley Research Center.
Contributors: Langley Research Center.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Series: NASA technical paper ; 1316; NASA technical paper -- 1316.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; for sale by the National Technical Information Service
Published: 1978
Place of publication: [Washington]; Springfield, Va
Language: eng
Number of pages: 76
Subjects: Guided missiles -- Design and construction.; Aerodynamics, Supersonic.
Notes: Sept. 1978.

Includes bibliographical references.