An Aerodynamic Layout of a Transatmospheric Reusable Vehicle
An aerodynamic layout and aircraft technology, applied in the field of aircraft, can solve the problems of cumbersome use and maintenance, expensive launch costs, etc., and achieve the effects of small structure quality, short launch preparation period, and reduced interference shock wave loss.
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[0028] The present invention will be further described below in conjunction with the accompanying drawings.
[0029] Such as figure 1 and figure 2 As shown, the layout of the transatmospheric reusable aircraft provided by the present invention includes a head 1, a fuselage 2, a horizontal wing 3, a vertical empennage 8, body flaps 5 and a liquid hydrogen / liquid oxygen linear plug nozzle rocket motor 6 . Two inclined horizontal wings 3 are arranged on both sides of the tail of the fuselage 2, two vertical empennages 8 are arranged on the back of the fuselage 2, and two body flaps 5 are also arranged on the lower surface of the fuselage 2 bottom. The liquid hydrogen / liquid oxygen linear plug nozzle rocket engine 6 is arranged at the tail position of the fuselage 2 . This layout has no booster, and a single stage can be launched from the ground into orbit, and can return to glide to land and be reused.
[0030] The rear edge of the horizontal wing 3 is provided with a roll a...
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