Liquid rocket system

TL;DR: In this article, a propulsion system in which pure hydrazine is used as the fuel for both a bipropellant rocket engine for high-thrust performance and in multiple monoppropellant thrusters for station keeping and attitude control functions is presented.

TL;DR: In this article, a radial motor powered by pressurized gas is described, which is used for starting the internal combustion engine of a portable implement such as a powered chain saw or lawn mower.

TL;DR: In this paper, an arrangement for the supply of propellant for the propulsion systems of a satellite has a main fuel tank, a main oxidizer tank and an additional or auxiliary tank.

TL;DR: In this paper, the authors describe an apparatus adapted to feed liquids by gas pressure, such as gasoline and liquid oxygen, at high pressure to a combustion chamber, in a rocket or other air-craft.