Wind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control
By: A. B. Blair, Jr.
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Series: NASA technical paper ; 1124; NASA technical paper -- 1124.
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: 101
Subjects: Airplanes -- Ramjet engines.; Spoilers (Airplanes); Rolling (Aerodynamics); Guided missiles -- Control systems.
Notes: Issued Mar. 1978.

Includes bibliographical references.