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  2. Kuznetsov NK-144 - Wikipedia

    en.wikipedia.org/wiki/Kuznetsov_NK-144

    The Kuznetsov NK-144 is an afterburning turbofan engine made by the Soviet Kuznetsov Design Bureau. Used on the early models of the Tupolev Tu-144 supersonic aircraft, it was very inefficient and was replaced with the Kolesov RD-36-51 turbojet engine.

  3. Category:Kuznetsov aircraft engines - Wikipedia

    en.wikipedia.org/wiki/Category:Kuznetsov...

    Kuznetsov NK-89; Kuznetsov NK-92; ... Kuznetsov TV-022; N. Kuznetsov NK-12; Kuznetsov NK-144 This page was last edited on 15 October 2020, at 18:55 ...

  4. Kuznetsov Design Bureau - Wikipedia

    en.wikipedia.org/wiki/Kuznetsov_Design_Bureau

    Kuznetsov's most powerful aviation engine is the Kuznetsov NK-321 that propels the Tupolev Tu-160 bomber and was formerly used in the later models of the Tu-144 supersonic transport (an SST that is now obsolete and no longer flown). The NK-321 produced a maximum of about 245 kN (55,000 lb f) of thrust. Kuznetsov aircraft engines include:

  5. JSC Kuznetsov - Wikipedia

    en.wikipedia.org/wiki/JSC_Kuznetsov

    Kuznetsov's most powerful aviation engine is the Kuznetsov NK-321 that propels the Tupolev Tu-160 bomber and was formerly used in the later models of the Tu-144 supersonic transport (an SST that is now obsolete and no longer flown).

  6. Tupolev Tu-144 - Wikipedia

    en.wikipedia.org/wiki/Tupolev_Tu-144

    The only engine available in time with the required thrust and suitable for testing and perfecting the aircraft was the afterburning Kuznetsov NK-144 turbofan with a cruise SFC of 1.58 kg/kgp hr. Development of an alternative engine to meet the SFC requirement, a non-afterburning turbojet, the Kolesov RD-36-51A, began in 1964. [5]

  7. Kolesov RD-36 - Wikipedia

    en.wikipedia.org/wiki/Kolesov_RD-36

    RD-36-41 Created on the basis of the engine 'VD-19' . [2]Thrust – 16,150 kgf (35,600 lbf; 158,400 N) RD-36-51 This engine was a replacement for the Kuznetsov NK-144 turbofan used on the Tu-144D SST, giving an increase in full payload range from 3,080km to 5,330km. [3]

  8. Contra-rotating propellers - Wikipedia

    en.wikipedia.org/wiki/Contra-rotating_propellers

    The A-90 uses one NK-12 engine mounted at the top of its T-tail, along with two turbofans installed in the nose. In the 1980s, Kuznetsov continued to develop powerful contra-rotating engines. The NK-110, which was tested in the late 1980s, had a contra-rotating propeller configuration with four blades in front and four in back, like the NK-12.

  9. Nikolai Kuznetsov (engineer) - Wikipedia

    en.wikipedia.org/wiki/Nikolai_Kuznetsov_(engineer)

    [4] [5] Several stockpiled NK-33 engines were refurbished and modified by Aerojet and used for the Orbital Sciences Antares. [6] In the 1960s he developed aircraft engines specifically for the world's first supersonic transport aircraft to fly Tupolev Tu-144, the Kuznetsov NK-144 turbofan.