Effect of aerodynamic and angle-of-attack uncertainties on the May 1979 entry flight control system of the space shuttle from Mach 8 to 1.5
By: Howard W. Stone and Richard W. Powell
Contributors: Powell, Richard W; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch; Langley Research Center
Series: NASA technical paper -- 2365
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1985
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 133
Subjects: Space vehicles -- Control systems; Space vehicles -- Atmospheric entry; Space shuttles
Notes: "Langley Research Center."

Distributed to depository libraries in microfiche

"January 1985"--Cover

Subject category 16

Includes bibliographical references