User:Meisam.hajipour/sandbox

Expansion rocket Propulsion

This type of engine is one of the liquid fuel engines, but with a much simpler building and Very low cost. The most important difference between this type of propulsion and liquid fuel engine in the building is its fuel tanks, so that the fuel tanks are turned into several parts by a tube or a diagram. In conventional liquid fuel engines, the right fuel pressure for injection into the injector and combustion chamber is provided by the gas turbine, but in expansion propulsion, the gas-generating turbines have been deleted. As a result, the fluid pressure is supplied by compressed air inside the tank and behind the fuel.

The most important difference between this type of propulsion and liquid fuel engine in the building is its fuel tanks, so that the fuel tanks are turned into several parts by a tube or a diagram.In this type of propulsion, fuel can be combined directly with oxidant or placed in independent tanks. Diaphragm propulsion has the characteristics of both liquid and solid fuel engines. This means that the building is very simple and light in weight and is a public and affordable liquid fuel. In solid fuel engines, a small amount of solid fuel after combustion is converted into a large volume of gas and smoke with very high temperatures, which is the most important factor in the identification of rockets by defense systems.

applications - Use in short-range portable guided missiles such as launch showers, anti-tank and anti-tank and anti-helicopter systems - Use in balance and control systems for large missiles, satellites and other space cargoes (manual maneuvering system)