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  2. Kuznetsov NK-32 - Wikipedia

    en.wikipedia.org/wiki/Kuznetsov_NK-32

    A non-afterburning variant known as NK-32 Tier 2 for Tu-160 and NK-65 will be used in the upcoming Russian bomber, PAK DA. [ 1 ] NK-65 and a geared high-bypass turbofan variant PD-30 , with a thrust of 30,000 kilograms-force (290 kN; 66,000 lbf) has been proposed for use on new Russian wide-body airliners, as well as the upgraded Antonov An-124 ...

  3. Kuznetsov Design Bureau - Wikipedia

    en.wikipedia.org/wiki/Kuznetsov_Design_Bureau

    The Kuznetsov Design Bureau also produced the Kuznetsov NK-87 turbofan engine that was used on the Lun-class ekranoplan. (Only one such aircraft has ever been produced.) [citation needed] 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 ...

  4. JSC Kuznetsov - Wikipedia

    en.wikipedia.org/wiki/JSC_Kuznetsov

    The Kuznetsov Design Bureau also produced the Kuznetsov NK-87 turbofan engine that was used on the Lun-class ekranoplan. (Only one such aircraft has ever been produced.) 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 ...

  5. NK-321 - Wikipedia

    en.wikipedia.org/?title=NK-321&redirect=no

    Language links are at the top of the page across from the title.

  6. Kuznetsov NK-25 - Wikipedia

    en.wikipedia.org/wiki/Kuznetsov_NK-25

    The Kuznetsov NK-25 is a turbofan aircraft engine made by the Soviet Kuznetsov Design Bureau and used in the Tupolev Tu-22M strategic bomber. One of the most powerful supersonic engines in service today, it is rated at 245 kN (55,000 lbf) thrust. The three shaft engine was designed in the years 1972–1974.

  7. Nikolai Kuznetsov (engineer) - Wikipedia

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

    It proved to be a successful engine and was completed in 1955. The new turboprop engine, named Kuznetsov NK-12, displayed great performance and was developed up to 11,000 kW. It was used in the Antonov An-22 aircraft, A-90 Orlyonok Ekranoplane and the Tupolev Tu-95 strategic bomber among others. The later models produced around 15,000 kW.

  8. 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]

  9. 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.