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Rocket Propulsion Types

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Nuclear Thermal Propulsion

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Heats a propellant like hydrogen using a nuclear reactor. The hot gas is then expelled through a nozzle to produce thrust.

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Nuclear Electric Propulsion

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Generates electrical power from a nuclear reactor to drive an electric propulsion system like an ion or Hall-effect thruster.

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Pulsed Plasma Thruster

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Utilizes electrical energy to ionize a solid propellant and create plasma, which is then expelled by magnetic fields to generate thrust.

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Magnetoplasmadynamic (MPD) Thruster

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Generates thrust by the acceleration of plasma through the Lorentz force, which is the force exerted by magnetic fields on moving charged particles.

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Electric or Ion Propulsion

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Accelerates ions using electricity (often from solar panels) to create thrust. The propellant, usually xenon, is ionized then expelled by electric or magnetic fields.

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Chemical Propulsion

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Uses the reaction of chemical propellants (fuel and oxidizer) to produce hot gas that is expelled through a nozzle to generate thrust.

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Hybrid Propulsion

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Combines elements of solid and liquid propulsion. A solid fuel reacts with a liquid or gaseous oxidizer to produce thrust.

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Cold Gas Propulsion

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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.

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Solid Rocket Propulsion

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Employs solid propellants that ignite to form a high-pressure and high-temperature gas that is expelled through a nozzle to create thrust.

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Air-breathing Rockets

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Utilizes atmospheric oxygen from the Earth's atmosphere as the oxidizer as opposed to carrying an onboard supply.

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