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The Kuznetsov NK-93 was a civilian aircraft engine, a hybrid between a turbofan and a turboprop known as a propfan. The engine was also unique in having a separate duct around the contra-rotating propellers , as most other propfans are unducted.
Download QR code; Print/export Download as PDF; Printable version; In other projects Wikimedia Commons; ... Kuznetsov NK-89; Kuznetsov NK-92; Kuznetsov NK-93 ...
Kuznetsov NK-92 turbofan (modified to NK-93 further on). 220 to < 350 kN; Kuznetsov NK-93 propfan. Projected to power the Il-96, Tu-204, and Tu-330. Kuznetsov NK-114 Ekranoplanes and aircraft engines; Kuznetsov NK-116 Beriev Be-2500 Neptun engine; Kuznetsov NK-144 afterburning turbofan. Powered the early models of the Tupolev Tu-144 supersonic ...
The primary engines for the development rockets were Kuznetsov NK-15 and Kuznetsov NK-15V (later developed into Kuznetsov NK-33 and Kuznetsov NK-43). Ultimately, these designs were successful but arrived too late. By the time the bugs in this very advanced design were rectified, the N1 rocket program had been cancelled.
This Bureau also produced the Kuznetsov NK-144 afterburning turbofan engine. This engine powered the early models of the Tupolev Tu-144 SST. 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]
The NK-92 was proposed to power the Ilyushin Il-106 heavy military transport aircraft. Development of the Il-106 aircraft and its NK-92 engine slowed in the early 1990s. However, aspects of the engine's design were applied to the NK-92's civil engine counterpart, the Kuznetsov NK-93, which was tested in flight in the first decade of the 2000s. [1]
Documentary video on Russian rocket engine development of the NK-33 and its predecessors for the N1 rocket. (NK-33 story starts at 24:15–26:00 (program shuttered in 1974); the 1990s resurgence and eventual sale of the remaining engines from storage starts at 27:25; first use on a US rocket launch in May 2000.) NK-33's specifications
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 ...
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