Device for reducing aerodynamic drag
A technology of aerodynamic resistance and engines, applied in the field of aerospace vehicles, can solve the problems of reducing payload, difficulty in using space shuttles, and designing bulky release devices, etc.
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[0021] The present invention proposes a device for reducing the aerodynamic drag of aircraft 1 (such as space shuttles and space launchers).
[0022] The principle of the invention is to adopt a passive device that can be eliminated by the rocket engine itself after the rocket engine is ignited. The non-powered device can also provide a very light solution and achieve reliability through its design.
[0023] The device of the present invention is designed to allow the rocket engine to properly ignite and completely clear the device after ignition, thereby avoiding the risk of debris falling to the ground.
[0024] figure 1 The example shown is a space shuttle equipped with at least one engine 2 equipped with jet tube propulsion nozzles 3 projecting over the rear of the space shuttle fuselage 4.
[0025] As is conventionally known, the propulsion nozzle of the jet tube of the engine becomes wider as it leaves the rear of the aircraft fuselage.
[0026] The shielding device includes at l...
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