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  2. Air turborocket - Wikipedia

    en.wikipedia.org/wiki/Air_turborocket

    The air turboramjet engine is a combined cycle engine that merges aspects of turbojet and ramjet engines. [2] The turboramjet is a hybrid engine that essentially consists of a turbojet mounted inside a ramjet. The turbojet core is mounted inside a duct that contains a combustion chamber downstream of the turbojet nozzle.

  3. Aerojet Rocketdyne AR1 - Wikipedia

    en.wikipedia.org/wiki/Aerojet_Rocketdyne_AR1

    Aerojet Rocketdyne proposed in 2014 to "lobby the government to fund an all-new, U.S.-sourced rocket propulsion system." In June 2014, Aerojet initially projected it would cost under US$25 million per pair of engines, not including the up to US$1 billion estimated development cost to be funded by the government.

  4. PAC MFI-17 Mushshak - Wikipedia

    en.wikipedia.org/wiki/PAC_MFI-17_Mushshak

    Azerbaijani Air and Air Defence Force – 10 [5] [6] Iran. Iran Air Force – 25 [7] Iraq. Iraqi Air Force - 12 MFI-395 Super Mushshak delivered (additional 12 on order). 2nd batch of two aircraft delivered on 19 April 2023 to 202nd Training Squadron at Balad Air Base, Iraq. [8] Nigeria. Nigerian Air Force – 10 delivered as of January 2018. [9]

  5. Air-augmented rocket - Wikipedia

    en.wikipedia.org/wiki/Air-augmented_rocket

    The effectiveness of this simple method can be dramatic. Typical solid rockets have a specific impulse of about 260 seconds (2.5 kN·s/kg), but using the same fuel in an air-augmented design can improve this to over 500 seconds (4.9 kN·s/kg), a figure unmatched even by high specific impulse hydrolox engines.

  6. Rocket turbine engine - Wikipedia

    en.wikipedia.org/wiki/Rocket_turbine_engine

    A rocket turbine engine is a combination of two types of propulsion engines: a liquid-propellant rocket and a turbine jet engine. Its power-to-weight ratio is a little higher than a regular jet engine, and works at higher altitudes. [1] [2] [3]

  7. Microturbo TRI 60 - Wikipedia

    en.wikipedia.org/wiki/Microturbo_TRI_60

    The Microturbo TRI 60 is a small, expendable turbojet engine developed for use in cruise missiles, target drones, and other small unmanned air vehicles. Variants of this engine produce from 3.5 to 5.3 kN (790 to 1,190 lbf) of thrust. The engine first ran in 1974.

  8. Popeye (missile) - Wikipedia

    en.wikipedia.org/wiki/Popeye_(missile)

    The standard Popeye and smaller Popeye-Lite are powered by a single-stage solid rocket. Rafael offered a Popeye Turbo air launched variant featuring a jet engine and folding wings for a UK competition specifying a cruise missile with range of at least 320 km (200 mi) in 1994; publicly exposing a lowest possible maximum range for that variant.

  9. Klimov RD-33 - Wikipedia

    en.wikipedia.org/wiki/Klimov_RD-33

    According to Air Commodore Mehmood engines are solid and reliable: “We’ve flown 7,000 hours with the engine and we haven’t had any problems”, he said. [7] [8] The RD-93MA is an upgrade of the RD-93 engine. The thrust of the RD-93MA is expected to 9300 kgf compared to 8300 kgf of the RD-93, a significant bump-up in power which will help ...