Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration
By: W.P. Phillips and W.C. Engelund.
Contributors: Engelund, W. C.; United States. National Aeronautics and Space Administration.
Series: NASA TM -- 111926; AIAA -- 95-1848; NASA technical memorandum -- 111926..
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1997
Place of publication: [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Aerodynamic characteristics.; Spacecraft configurations.; Subsonic speed.; Supersonic speed.; Hypersonics.; Single stage to orbit vehicles.; Longitudinal stability.; Controllability.
Other titles: Subsonic to hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 97-0681-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.