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Rocket Propulsion Types
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Nuclear Thermal Propulsion
Heats a propellant like hydrogen using a nuclear reactor. The hot gas is then expelled through a nozzle to produce thrust.
Nuclear Electric Propulsion
Generates electrical power from a nuclear reactor to drive an electric propulsion system like an ion or Hall-effect thruster.
Pulsed Plasma Thruster
Utilizes electrical energy to ionize a solid propellant and create plasma, which is then expelled by magnetic fields to generate thrust.
Magnetoplasmadynamic (MPD) Thruster
Generates thrust by the acceleration of plasma through the Lorentz force, which is the force exerted by magnetic fields on moving charged particles.
Electric or Ion Propulsion
Accelerates ions using electricity (often from solar panels) to create thrust. The propellant, usually xenon, is ionized then expelled by electric or magnetic fields.
Chemical Propulsion
Uses the reaction of chemical propellants (fuel and oxidizer) to produce hot gas that is expelled through a nozzle to generate thrust.
Hybrid Propulsion
Combines elements of solid and liquid propulsion. A solid fuel reacts with a liquid or gaseous oxidizer to produce thrust.
Cold Gas Propulsion
Employs a pressurized inert gas that expands and is expelled through a nozzle to produce thrust, commonly used for small attitude adjustments or station keeping.
Solid Rocket Propulsion
Employs solid propellants that ignite to form a high-pressure and high-temperature gas that is expelled through a nozzle to create thrust.
Air-breathing Rockets
Utilizes atmospheric oxygen from the Earth's atmosphere as the oxidizer as opposed to carrying an onboard supply.
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