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公开(公告)号:WO2022259138A1
公开(公告)日:2022-12-15
申请号:PCT/IB2022/055282
申请日:2022-06-07
IPC分类号: F02K99/00
摘要: The invention relates to a closed-circuit space shuttle used for interplanetary and interstellar transport and to capturing solar energy, being a constructive combination between rocket and aircraft in which the take-off and landing are made vertically, and the vertical take-off does not last more than a minute, after which the space shuttle is driven like an airplane using the load-bearing force generated by the 9 wings that support the four rockets of the space shuttle, the airplane regime being possible due to the atmosphere of the planet in which it is, excepting only the Earth satellite which has a gravity of 0.17 G, but has no atmosphere, for the correct operation of the shuttle its acceleration must be greater than 0.1 G, and 1G being the gravity of the Earth. The shuttle, according to the invention, is powered only from the outside with only solar energy and energy from laser cannons, being recommended to use laser cannons or thousands of mirrors that focus the sun's rays during takeoff until the exit into outer space on the shuttle, which together with the friction will heat the outer surface of the space shuttle and for a homogeneous heating of the entire surface of the shuttle must rotate around its axis two or three times a minute, use laser cannons during takeoff until the exit in space, giving the possibility to reduce the amount of fuel on board the ship which will be 20 times smaller to put the shuttle in space on our planet, the propulsion system being made by 19 double rocket engines, (ie rocket in rocket). The inner rocket works by burning hydrogen and oxygen, and the outer rocket concentrically is fed by high pressure steam that washes the inner rocket accumulating an even higher thermal energy, respectively, kinetic, the shuttle has four more rockets, having a total of 76 double rocket engines.