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    Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept (1995)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: A 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.
    Keywords: AERODYNAMICS
    Type: NASA-TM-108489 , NAS 1.15:108489
    Format: application/pdf
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