Plasma Detonation Engine (PDE) is a new development in the field of rocket engines. It uses plasma explosions to generate thrust.
The plasma subsidy engine circuit includes the following main components:
1. Combustion chamber: the main element of the engine in which plasma generation and its subsidization takes place. The combustion chamber has numerous openings through which the plasma exits and creates thrust.
2. Fuel supply: Fuel is supplied to the combustion chamber from a tank located on the rocket. It is important that the fuel supply is accurate and stable to ensure reliable engine operation.
3. Fuel regulator: a device that controls the supply of fuel to the combustion chamber. It allows you to regulate and maintain optimal conditions for fuel combustion and plasma generation. Gorenje
4. Electrodes: metal conductors that are installed in the combustion chamber and are responsible for initiating and controlling plasma explosions. The electrodes create electrical discharges that ignite a mixture of fuel and air, forming a plasma.
5. Reactor: a device that is designed to provide plasma. The reactor directs the plasma column in the right direction and amplifies the plasma energy, which ensures more efficient thrust generation.
6. Cooling system: The plasma subsidized engine generates a significant amount of heat, so a cooling system is needed to prevent overheating and damage to engine components. This may include a coolant circulation system or the use of heat exchangers.
