Aerodynamic test and analysis of a turbojet-boosted launch vehicle concept (spacejet) over a Mach number range of 1.50 to 2.86
By: Gregory D. Riebe, William J. Small, and Odell A. Morris.
Contributors: Small, William J.; Morris, Odell A.; Langley Research Center.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Series: NASA technical paper -- 1888.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1981
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 52
Subjects: Aerodynamics, Supersonic.; Winged spacecraft.
Notes: "Langley Research Center."

Subject category 02.

"July 1981"--Cover.

Includes bibliographical references.