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