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  2. IAE V2500 - Wikipedia

    en.wikipedia.org/wiki/IAE_V2500

    The engine's name is a combination of the Roman numeral V, symbolizing the five original members of the International Aero Engines consortium, which was formed in 1983 to produce the V2500 engine. The 2500 represents the 25,000- pound-force (110 kN) produced by the original engine model, the V2500-A1.

  3. International Aero Engines - Wikipedia

    en.wikipedia.org/wiki/International_Aero_Engines

    IAE's current purpose is the development, production and aftermarket services of the V2500 aero engine family, which powers the Airbus A320 family and McDonnell Douglas MD-90 aircraft. IAE also supplies the V2500-E5 to power the Embraer KC-390 military transport aircraft; this arrangement is the first military application of the engine. [18]

  4. IAE SuperFan - Wikipedia

    en.wikipedia.org/wiki/IAE_SuperFan

    The IAE V2500SF SuperFan was a design study for a high-bypass geared turbofan derived from the IAE V2500.It was offered as the primary engine option for the Airbus A340-200 and 300 in January 1987.

  5. Japanese Aero Engine Corporation - Wikipedia

    en.wikipedia.org/wiki/Japanese_Aero_Engine...

    The V in V2500 denotes the five original partners, whilst 2500 symbolizes the original thrust level of 25000 lb f. FiatAvio later withdrew from the V2500 consortium. [2] Workshare on the joint venture's first engine, the V2500, was divided between the constituent aero-engine companies.

  6. List of aircraft engines - Wikipedia

    en.wikipedia.org/wiki/List_of_aircraft_engines

    ABLE 2500; ABLE VW x 2 Geared Drive; Accurate Automation Corp. Accurate Automation AT-1500; ... Piston Engines [3] Armstrong Siddeley Terrier; Armstrong Siddeley Mastiff;

  7. Klimov VK-2500 - Wikipedia

    en.wikipedia.org/wiki/Klimov_VK-2500

    Rated at 2,500 shp (1,864 kW) take-off power. Powers Mi-28NM. [2] VK-2500M Next generation derivative of VK-2500 under development by Klimov, with planned reduced fuel burn and weight. Rated at 2,600 shp (1,939 kW) for take-off and 2,200 shp (1,641 kW) continuous power. Deliveries planned by 2023. [4] TV3-117VMA-SB3 Ukrainian designation for VK ...

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    mail.aol.com

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  9. Comparison of orbital rocket engines - Wikipedia

    en.wikipedia.org/wiki/Comparison_of_orbital...

    Engine Origin Designer Vehicle Status Use Propellant Power cycle Specific impulse (s) [a] Thrust (N) [a] Chamber pressure (bar) Mass (kg) Thrust: weight ratio [b] Oxidiser: fuel ratio