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High-Frequency Detonation-Driven Engine Utilizing High-Voltage Pulsed Plasma

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Abstract During the operation of a fuel detonation engine, oxygen is required for combustion to provide the necessary support. After the combustion process, the oxygen content in the gas decreases, making it difficult to form a multistage supercharging system. However, in this work, when the plasma is heated, it can still be reheated and detonated, allowing for the creation of a multistage detonation continuous supercharging engine. The generation of high-temperature plasma does not have strict requirements for the composition of the gas; it does not require a very high content of oxygen or other types of combustion-supporting agents. Nor does it necessarily need standard atmospheric pressure or higher gas pressure support; it can be applicable in a certain degree of vacuum. To verify the feasibility of the output thrust of the high-frequency plasma detonation engine, the author conducted tests on a single-module plasma detonation engine in a certain vacuum environment. By the action of high-frequency and high-voltage plasma pulse heating, a single-stage ion engine can achieve a jet velocity far exceeding the speed of sound. These findings demonstrate that the detonation plasma engine has extremely promising prospects for future practical applications.
Title: High-Frequency Detonation-Driven Engine Utilizing High-Voltage Pulsed Plasma
Description:
Abstract During the operation of a fuel detonation engine, oxygen is required for combustion to provide the necessary support.
After the combustion process, the oxygen content in the gas decreases, making it difficult to form a multistage supercharging system.
However, in this work, when the plasma is heated, it can still be reheated and detonated, allowing for the creation of a multistage detonation continuous supercharging engine.
The generation of high-temperature plasma does not have strict requirements for the composition of the gas; it does not require a very high content of oxygen or other types of combustion-supporting agents.
Nor does it necessarily need standard atmospheric pressure or higher gas pressure support; it can be applicable in a certain degree of vacuum.
To verify the feasibility of the output thrust of the high-frequency plasma detonation engine, the author conducted tests on a single-module plasma detonation engine in a certain vacuum environment.
By the action of high-frequency and high-voltage plasma pulse heating, a single-stage ion engine can achieve a jet velocity far exceeding the speed of sound.
These findings demonstrate that the detonation plasma engine has extremely promising prospects for future practical applications.

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