Stability and control characteristics of a monoplanar missile configuration with triform-tail-fin arrangements at mach numbers from 1.70 to 2.86
By: Milton Lamb
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch; Langley Research Center
Series: NASA technical memorandum -- 83223
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1981
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 116
Subjects: Guided missiles -- Control systems -- Testing; Guided missiles -- Aerodynamics -- Testing; Wind tunnels -- Testing
Notes: "Langley Research Center."

"December 1981"--Cover

Subject Category 02

Bibliography: p. 10