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
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