Comparison of theoretical and experimental steady wing loads on a space shuttle configuration at Mach numbers of 0.6 and 1.4 /

Bibliographic Details

Main Author:	Preisser, John S.
Corporate Author:	United States. National Aeronautics and Space Administration
Other Authors:	Lowder, Harold E.
Format:	Government Document Book
Language:	English
Published:	Washington : National Aeronautics and Space Administration, 1977.
Series:	NASA technical memorandum ; NASA TM X-3404.
Subjects:	Reusable space vehicles.