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Extrusion cycle

Power cycle form of liquid rocket engine
Extrusion cycle pressure-fed cycle )Yes Liquid rocket engine A form of power cycle. The propellant is squeezed by high-pressure gas and enters the combustion chamber.
Chinese name
Extrusion cycle
Foreign name
Pressure-fed engine

brief introduction

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Extrusion cycle pressure-fed cycle )Yes Liquid rocket engine A form of power cycle. The propellant is squeezed by high-pressure gas and enters the combustion chamber.
The advantage of extrusion cycle is to avoid the complicated structure turbine , pumps and delivery pipes. Because the use of extrusion cycle can greatly reduce the cost and complexity of the engine. The disadvantage is that the pressure generated is not high enough, so Engine efficiency Not high.
American spacecraft often use this cycle, such as Apollo spacecraft Service module engine, lunar module engine and Attitude control engine [1]

Liquid rocket engine

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Liquid propellant rocket engine (English: Liquid Propellant Rocket Engine, abbreviated as LPRE) Liquid rocket engine or Liquid rocket engine , refers to the liquid Fuel and Oxidant As energy and working medium rocket engine The basic components of liquid rocket engine include Thrust chamber Propellant supply system and Engine control system Etc. Liquid propellant Storage Propellant tank When the engine is working, the propellant is delivered to the combustion chamber After atomization, evaporation, mixing and combustion to generate high-temperature and high-pressure gas nozzle Accelerate to Supersonic velocity Discharge, resulting in thrust
Liquid rocket engine The propellant used can be a liquid chemical, that is, monopropellant, or a combination of several liquid chemicals, that is, bipropellant and tripropellant, both of which have high energy characteristics. The commonly used monopropellant is hydrazine, which is mainly used for small thrust engines. Bipropellants mainly include liquid oxygen / liquid hydrogen Liquid oxygen/ Hydrocarbons kerosene gasoline and alcohol Etc.) nitric acid /Hydrocarbons Nitrogen tetroxide / Unsymmetrical dimethylhydrazine And other combinations.
The first liquid rocket in history was launched by an American rocket scientist Robert H. Goddard It was launched in 1926. German rocket experts Von Braun The research team of the Second World War Developed during V-2 rocket It has greatly promoted the development of large liquid rocket engines. After World War II, the United States, the Soviet Union/Russia and many other countries developed a large number of liquid rocket engines. As one of the most mature rocket propulsion systems, liquid rocket engine has high performance and many unique advantages, and is widely used in Carrier rocket , spacecraft and Missile Liquid rocket engines were also briefly used as aircraft Propulsion power. [1]

Gas generator cycle

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Gas generator Cycle( Gas-generator cycle )Also called Open cycle , Yes Binary liquid propellant rocket One of the power cycles of an engine. A small part of the propellant is burned in the gas generator to generate gas to drive the turbine pump of the engine.
Compared with similar Staged combustion cycle Gas generator Circulation has many advantages. The turbine of the gas cycle does not have to deal with the back pressure when it discharges exhaust gas into the combustion chamber, so the working efficiency of the turbine is higher, and the pressure supplied to the fuel is also greater, thus increasing the engine's Specific impulse Another advantage is that the turbine life of the gas cycle is longer and more reliable. some Reusable launch vehicle This power cycle has great advantages.
The main disadvantage of this cycle is the loss of efficiency. Because a part of the fuel is used to drive the turbine, and the exhaust gas is discharged directly, it is not like a graded combustion cycle in terms of net efficiency. [1]

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