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
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