Static aerodynamic characeristics of a winged single-stage-to-orbit vehicle at Mach numbers from 0.3 to 4.63
By: Delma C. Freeman, Jr. and Roger H. Fournier, Langley Research Center
Contributors: Fournier, Roger H., joint author; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office; Langley Research Center
Series: NASA technical paper ; 1233
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; for sale by the National Technical Information Service
Published: 1978
Place of publication: [Washington]; Springfield, Va
Language: eng
Number of pages: 116
Subjects: Space vehicles -- Atmospheric entry; Aerodynamics
Notes: Issued Aug. 1978

Includes bibliographical references