Static aerodynamic characteristics of a single-stage-to-orbit vehicle with low planform loading at Mach numbers from 0.3 to 4.63
By: Delma C. Freemand, Jr. and Roger H. Fournier.
Contributors: Fournier, Roger H.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Series: NASA technical memorandum ; 74056; NASA technical memorandum -- 74056.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; for sale by the National Information Service
Published: 1977
Place of publication: [Washington]; Springfield, Va
Language: eng
Number of pages: 66
Subjects: Stability of space vehicles.
Notes: Issued Nov. 1977.

Includes bibliographical references.