Rocket propellant
The rocket propeller is typically stored in a number of forms in the propeller vessel, which was used in the past to be ejected from the rocket engine in the form of a fluid ejection to produce thrust as propulsion. Fuel propellants are often combusted with oxidant propellants to produce large amounts of very hot gases. The gas is inflated and sprayed from the nozzle, accelerating, from the bottom of the rocket to produce thrust until the rocket reaches a very high speed. Sometimes the propellant does not burn, but can be heated from the outside to achieve better results. For smaller experimental propellers, the use of compressed gas is pushed through the propulsion nozzle to propel the spacecraft. Chemical rocket propellant is the most commonly used, the rocket through the exothermic chemical reaction to produce hot gas to achieve the purpose of propulsion. In the ion thruster, the propellant is a charged atom and is ejected from the tail of the spacecraft in a magnetic repulsion. However, the magnetically accelerated ion driver is generally not considered a rocket, but rather a similar-level propeller using electric heating and magnetic nozzles. ...