Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers
By: A.B. Blair, Jr., Jerry M. Allen, and Gloria Hernandez
Contributors: Allen, Jerry M; Hernandez, Gloria; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Series: NASA technical paper -- 2157
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1983
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 83
Subjects: Guided missiles -- Wings; Airplanes -- Wings, Canard; Aerodynamics, Supersonic
Notes: Distributed to depository libraries in microfiche

"June 1983"--Cover

Subject category 02

Includes bibliographical references