Effect of aerodynamic and angle-of-attack uncertainties on the blended entry flight control system of the space shuttle from Mach 10 to 2.5
By: Howard W. Stone and Richard W. Powell
Contributors: Powell, Richard W; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Series: NASA technical paper -- 2283
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1984
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 287
Subjects: Space vehicles -- Control systems; Space vehicles -- Atmospheric entry; Space shuttles
Notes: Distributed to depository libraries in microfiche

"April 1984"--Cover

Subject category 08

Includes bibliographical references