Antiproton rocket engine

Abstract

The invention discloses an antiproton rocket engine, which comprises an engine casing, an antiproton generator is installed at the front end of the engine casing, a nozzle assembly is arranged at the tail, and the middle section includes an antiproton extraction pipeline, an annihilation device, a heat conversion chamber and a storage chamber. air box. The gas storage box is fixedly installed on the inner wall of the engine housing. An annihilation device is installed on one side of the outer wall of the gas storage box. One end of the annihilation device is connected to the antiproton generator through the antiproton extraction pipeline, and the other end is connected to the heat conversion chamber. The engine casing is socketed with the nozzle assembly. The antiproton rocket engine disclosed by the invention has the advantages of high specific impulse, long life, fast speed, no pollution, high efficiency, etc., and can significantly increase the quality of payload when used for attitude control of deep space probes.

Description

technical field [0001] The invention belongs to the technical field of engines, in particular to an antiproton rocket engine. Background technique [0002] The rocket engine is an important part of the aircraft, and its main function is to provide the required power device for the accelerated orbit change and return and landing of missile weapons, launch vehicles and satellites. Although the current rocket engine has achieved relatively ideal results in form, there are still many problems in many aspects. The basic problems are: first, the specific impulse of traditional rocket engines is restricted, and conventional solid and liquid fuels The generated specific impulse has a bottleneck value; the second is that the operating conditions of the engine are limited. For solid ramjet engines and liquid ramjet engines, a certain amount of air capture must be provided by the outside to ensure efficient and reliable operation of the engine. Higher requirements are put forward for ...

AI Technical Summary

Problems solved by technology

Although the current rocket engine has achieved relatively ideal results in form, there are still many problems in many aspects. The basic problems are: first, the specific impulse of traditional rocket engines is restricted, and conventional solid and liquid fuels The generated specific impulse has a bottleneck value; the second is that the operating conditions of the engine are limited. For solid ramjet engines and liquid ramjet engines, a certain amount of air capture must be provided by the outside to ensure efficient and reliable operation of the engine. Higher requirements are put forward for the working height, working speed and flight attitude of the engine; third, most of the combustion products of rocket engines will affect the surrounding atmospheric environment and discharge harmful substances into the atmosphere

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