This invention concept pertains to a spacecraft propulsion system that uses Water (H₂O) and electrolysis, that separates the water into Hydrogen (H₂) and Oxygen (O₂) gas, to use as propellant fuel, in the actual nozzle of the propulsion system. The electrolysis actually occurs in the nozzle of the propulsion system, so the Hydrogen (H₂) and Oxygen (O₂) don’t need to be stored in separate tanks, and the process is very efficient.
There are motors or solenoids that move the propulsion system back and forth or side to side, to get the right angle of attack for the satellite’s or spacecraft’s propulsion system, at the time of movement of the satellite or spacecraft.
