his approach can not be used.
Our solution is to the intake port and the dynamic pressure of the air entering the combustor nozzle design small electric compressor variable opening degree is provided in the center of the engine inlet station. Takeoff,north face clearance women, narrowing the intake port, closing the air vents of the dynamic pressure, starting the compressor, the air is pressed into the combustion chamber, the fuel is injected,air max torch, in the complete combustion under the action of a strong microwave combustion system, provides the initial thrust, with speed increases, gradually expanding the air intakes, by computer simulation, when the speed reaches 420 km / h, gradually open dynamic pressure air vents, the thrust increases faster; speeds up to 15 times the speed of sound, can be turned off small compressor. The air pressure into the combustion chamber can rely on dynamic pressure. Since none of the turbine, the combustor exit temperature is not restricted, there microwave combustion system, full combustion of the gas temperature can greatly improve the efficiency of power generation of the plasma at a high temperature to be much higher. The vectored thrust the strength will be enhanced. We AL41F the combustor as a model for simulation. The result is amazing, and to increase the thrust can! Due to the cancellation of a complex and expensive turbo compressor system and to start the motor, to increase the air vents of the intake port and the dynamic pressure control means, and small electric compressor, the total weight of the e
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