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Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle conceptA proposed wing-body reusable launch vehicle was tested in the NASA Marshall Space Flight Center's 14 x 14-inch trisonic wind tunnel during the winter of 1994. This test resulted in the vehicle's subsonic and transonic, Mach 0.3 to 1.96, longitudinal and lateral aerodynamic characteristics. The effects of control surface deflections on the basic vehicle's aerodynamics, including a body flap, elevons, ailerons, and tip fins, are presented.
Document ID
19950024291
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Springer, A. M.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1995
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-108489
NAS 1.15:108489
Accession Number
95N30712
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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