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Preliminary Aerodynamic Design of a Reusable Booster Flight Experiment
The Reusable Flight Experiment (ReFEx) is an experimental vehicle currently in development by the German Aerospace Center (DLR), which simulates the reentry of a winged reusable booster stage. The topic covered in this paper is the aerodynamic design through the Mach number range from 6.0 to 0.6, in
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