A proposed wing body reusable launch vehicle was tested in the Marshall Space Flight Center (MSFC) 14 x 14 inch trisonic wind tunnel during the winter of 1994. this test resulted in the vehicle's subsonic and transonic (Mach 03 to 1.96) longitudinal and lateral aerodynamic characteristics. The effects of control surface deflections on the basic vehicle aerodynamics including a body flap, elevons, ailerons, and tip fins are presented.
Transonic Aerodynamic Characteristics of a Proposed Wing Body Reusable Launch Vehicle Concept
1996
18 pages
Report
Keine Angabe
Englisch
Transonic Aerodynamic Characteristics of a Proposed Wing Body Reusable Launch Vehicle Concept
British Library Conference Proceedings | 1996
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