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Liquid Rocket Engines

Liquid rocket engines are propulsion systems that use liquid fuel and an oxidizer to produce thrust. When these two components are burned in a combustion chamber, they create high-speed gas that is expelled through a nozzle, generating the force needed to lift a rocket into space. The combination of fuels can vary, but they are typically mixed right before combustion to ensure efficient and controlled reactions. Liquid rocket engines provide advantages in terms of fuel efficiency and throttle control compared to solid fuel engines, making them ideal for missions requiring precision and adaptability throughout the flight.

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    Liquid rocket engines generate thrust by burning liquid propellants, typically a fuel and an oxidizer, in a combustion chamber. The combustion produces hot gases that expand and are expelled through a nozzle, propelling the rocket upwards. These engines are notable for their precise control, allowing for variable thrust levels and engine restarts. They are commonly used in space exploration, powering everything from satellites to crewed missions. The combination of efficiency and adaptability makes liquid rocket engines a fundamental technology in modern rocketry.