05 - Propulsion
DESIGN OF A WIND TUNNEL MODEL FOR A REUSABLE LAUNCH VEHICLE DURING ITS LANDING BURN
A.T. Hoang¹, N.J. Lawson¹, T. Bykerk, German Aerospace Center (DLR), Germany; ¹The University of Sydney, Australia
This paper presents the design and measurements from a wind tunnel model of a reusable launch vehicle (RLV) during its landing burn. The model of the body and supersonic nozzle will be tested in a low-speed wind tunnel, and aerodynamic data with a freestream Mach number <0.15 will be presented.rn