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  2. Rotating detonation engine - Wikipedia

    en.wikipedia.org/wiki/Rotating_detonation_engine

    This engine produced 4,000 lbf (18 kN) of thrust. NASA has stated their intention to create a 10,000-pound-force (44 kN) thrust unit as the next research step. [17] On December 20, 2023, a full-scale Rotating Detonation Rocket Engine combustor was reportedly fired for 251 seconds, achieving more than 5,800-pound-force (26 kN) of thrust.

  3. Pulse detonation engine - Wikipedia

    en.wikipedia.org/wiki/Pulse_detonation_engine

    A pulse detonation engine (PDE) is a type of propulsion system that uses detonation waves to combust the fuel and oxidizer mixture. [1][2] The engine is pulsed because the mixture must be renewed in the combustion chamber between each detonation wave and the next. Theoretically, a PDE can operate from subsonic up to a hypersonic flight speed of ...

  4. Pressure gain combustion - Wikipedia

    en.wikipedia.org/wiki/Pressure_gain_combustion

    This process is known as nuclear pulse propulsion and is stylistically similar to the pulse detonation engine. [6] PGC powered aircraft. In the mid-20th century, US aeronautical scientists and engineers were trying to study the properties of detonation waves. To do this, a primitive rotating detonation chamber of created.

  5. Propfan - Wikipedia

    en.wikipedia.org/wiki/Propfan

    A propfan, also called an open rotor engine, open fan engine[1][2] or unducted fan (as opposed to a ducted fan), is a type of aircraft engine related in concept to both the turboprop and turbofan, but distinct from both. The design is intended to offer the speed and performance of a turbofan, with the fuel economy of a turboprop.

  6. Components of jet engines - Wikipedia

    en.wikipedia.org/wiki/Components_of_jet_engines

    Components of jet engines. Diagram of a typical gas turbine jet engine. Air is compressed by the compressor blades as it enters the engine, and it is mixed and burned with fuel in the combustion section. The hot exhaust gases provide forward thrust and turn the turbines which drive the compressor blades. 1.

  7. Valveless pulsejet - Wikipedia

    en.wikipedia.org/wiki/Valveless_Pulsejet

    That is sucked in before any additional oxygen is sucked in. Of course, the air intake pipe has already supplied the oxygen by that point and the pulse reignites. A valveless pulsejet (or pulse jet) is the simplest known jet propulsion device. Valveless pulsejets are low in cost, light weight, powerful and easy to operate.

  8. Turbojet - Wikipedia

    en.wikipedia.org/wiki/Turbojet

    Rotating detonation engine; Ramjet. ... became the world's first aircraft to fly using the thrust from a turbojet engine. It was flown by test pilot Erich Warsitz. [9

  9. Aerospike engine - Wikipedia

    en.wikipedia.org/wiki/Aerospike_engine

    The aerospike engine is a type of rocket engine that maintains its aerodynamic efficiency across a wide range of altitudes. [1] It belongs to the class of altitude compensating nozzle engines. [2] Aerospike engines were proposed for many single-stage-to-orbit (SSTO) designs. They were a contender for the Space Shuttle main engine.