Bipropellantteihin
Bipropellantteihin refers to a type of rocket propellant system that utilizes two separate components, a fuel and an oxidizer, which are mixed and combusted in a rocket engine to produce thrust. This is in contrast to monopropellant systems, which use a single substance that decomposes or reacts to generate thrust. Bipropellant systems are widely used in rocketry due to their higher performance capabilities compared to monopropellants.
The two components of a bipropellant system are stored in separate tanks and are fed to the
Common bipropellant combinations include liquid hydrogen and liquid oxygen (LH2/LOX), which offer very high specific impulse