Kuznetsov Design Bureau

The Kuznetsov Bureau first became notable for producing the monstrous Kuznetsov NK-12 turboprop engine that powered the Tupolev Tu-95 bomber beginning in 1952 as a development of the Junkers 0022 engine. The new engine eventually generated about 15,000 horsepower (11.2 megawatts) and it was also used in the large Antonov An-22 Soviet Air Force transport.

Kuznetsov also produced the Kuznetsov NK-8 turbofan engine in the {{convert|90|kN|abbr=on}} class that powered the Ilyushin Il-62 and Tupolev Tu-154 airliners. This engine was next upgraded to become the about {{convert|125|kN|abbr=on}} Kuznetsov NK-86 engine that powered the Ilyushin Il-86 aircraft. 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|date=July 2024}}

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 {{convert|245|kN|abbr=on}} of thrust.

Kuznetsov aircraft engines include:

• RD-12 turbojet.
• RD-14 turbojet.
• RD-20 turboprop. BMW 003; powered the MiG-9.
• TV-022 turboprop. Reproduction of the Junkers Jumo 022.
• TV-2 turboprop. Improved version of TV-022.
• NK-4 turboprop. Powered the early Antonov An-10 and Ilyushin Il-18.
• NK-6 afterburning turbofan. Tested on the Tupolev Tu-95LL and was considered for the Tupolev Tu-22 and Tupolev Tu-123, but this never happened.
• NK-8 turbofan. Powers the original Ilyushin Il-62, A-90 Orlyonok ekranoplan and the Tupolev Tu-154A and B models.
• NK-12 contra rotating turboprop. Powers all the versions of the Tupolev Tu-95, Tupolev Tu-114, Tupolev Tu-126, Antonov An-22 and the A-90 Orlyonok ekranoplan. Initially designated as TV-12, but renamed to NK-12 in honor of company founder Nikolai Kuznetsov.
• NK-14 nuclear-powered engine. Powered the inboard engine of the prototype Tupolev Tu-119 nuclear-powered aircraft; a modified version of the Tupolev Tu-95.
• NK-16 turboprop. Was to power the Tupolev Tu-96.
• NK-22 afterburning turbofan. Powered the Tupolev Tu-22M0, M1 and M2.
• NK-25 afterburning turbofan. Powers the Tupolev Tu-22M3.
• NK-26 turboprop. Intended for ekranoplans.
• NK-32 afterburning turbofan. Powers the Tupolev Tu-160 and the later models of the Tupolev Tu-144.

: NK-321 (136 kN cruise {{Cite web|url=http://www.airwar.ru/enc/engines/nk321.html|title = Турбореактивный двухконтурный двигатель с форсажной камерой НК-321}} 245 kN, NK321M 280 to 300/350 kN, max 386)

: NK-32-02 for An-124 Tu-160 and PAK DA

• Kuznetsov PD-30, a geared high-bypass turbofan variant for the An-124 transport or airliners, derived from the NK-32 300 kN (max 328/350)
• NK-34 projectural turbojet. Intended for seaplanes.
• NK-44 turbofan. 400 kN (max up to 450 kN)
• NK-46 turbofan. Cryogenic design intended to power the Tupolev Tu-306 (a 450-seat derivative of the Tu-304).
• NK-56 turbofan. Was to power the Ilyushin Il-96, but was cancelled in favor of the Aviadvigatel PS-90.
• NK-62 propfan. Sporting contra-rotating propellers (four blades per propeller) of {{cvt|4.7|m|ftin}} in diameter, the engine had a thrust of {{cvt|245|kN|kgf lbf}} and a thrust-specific fuel consumption (TSFC) of {{cvt|0.288|tsfc}} at takeoff. The NK-62 was the most powerful turboprop or propfan ever built, though it never entered service. Tested from 1982 to 1990, the engine was designed for a cruise speed of Mach 0.75 at an altitude of {{cvt|11000|m|ft}}. Cruise thrust was {{cvt|44.1|kN|kgf lbf}}, and cruise TSFC was {{cvt|0.48|tsfc}}. The NK-62 was briefly considered for early designs of the Antonov An-70{{cite magazine |url=http://www.ozakaz.ru/index.php/articles/15032008/229-n2011-03-28-0338 |language=Russian |title=ОРЛИНЫЙ ГЛАЗ ФЛОТА Самолет радиолокационного дозора и наведения Як-44Э |trans-title=Eagle eye fleet: Yak-44E radar patrol and guidance aircraft |date=March 2008 |number=18 |given=Vadim |surname=Abidin |magazine=Oboronnyy Zakaz (Defense Order) |via=A.S. Yakovlev design bureau, Kryl'ia Rodiny (Wings of the Motherland) magazine |archive-url=https://web.archive.org/web/20190518064427/http://www.yak.ru/DOCS/Yak-44E.pdf |url-status=live |archive-date=May 18, 2019}} and for a re-engine of the Antonov An-124.
• NK-62M propfan. Developed in 1985–1987, this {{cvt|4850|kg|lb|adj=mid|engine}} was an uprated {{cvt|285.2|kN|kgf lbf}} thrust version of the NK-62, with {{cvt|314.7|kN|kgf lbf}} of emergency thrust available. Its TSFC was {{cvt|0.28|–|0.29|tsfc}} during takeoff and {{cvt|0.45|tsfc}} during cruise.{{cite magazine |language=Russian |year=2018 |number=1 |volume=115 |pages=20–24 |given=V. A. |surname=Zrelov |title=РАЗРАБОТКа ДВИГАТЕЛЕЙ "НК" БОЛЬШОЙ ТЯГИ НА БАЗЕ ЕДИНОГО ГАЗОГЕНЕРАТОРА |trans-title=Development of 'NK' large thrust engines on the basis of a single gas generator |magazine=Dvigatel |url=http://engine.aviaport.ru/issues/115/pics/pg20.pdf}} The engine was proposed for use on the Myasishchev M-90 giant detachable aircraft.{{cite web |url-status=live |archive-date=August 18, 2013 |archive-url=https://web.archive.org/web/20130818035509/http://alternathistory.org.ua/aviatsionnaya-sistema-mgs-mnogotselevoy-samolet-m-90okb-myasishcheva |url=http://alternathistory.com/aviatsionnaya-sistema-mgs-mnogotselevoj-samolet-m-90-okb-myasishheva/ |language=Russian |title=Авиационная система МГС-многоцелевой самолет М-90.ОКБ Мясищева |trans-title=Aviation system MGS-multipurpose aircraft M-90.OKB Myasishchev.}}
• NK-63 propfan. Ducted propfan based on the NK-32.{{cite web |url=http://www.leteckemotory.cz/motory/nk-62/ |language=Czech |title=NK-62, NK-63 - Kuznetsov, USSR}}
• NK-64 turbofan. 350 kN intended for Tu-204
• NK-65 turbofan. Intended for PAK DA
• NK-74 270 kN engine for a modified Tu-160 for extended range
• NK-86 turbofan. Upgraded version of the NK-8, powers the Ilyushin Il-86.
• NK-87 turbofan. Based on the NK-86, powers the Lun-class ekranoplan.
• NK-88 experimental turbofan. Powers the Tupolev Tu-155 hydrogen and LNG powered aircraft.
• NK-89 experimental turbofan. Was to power the unbuilt Tupolev Tu-156.
• NK-92 turbofan (modified to NK-93 further on). 220 to < 350 kN
• NK-93 propfan. Ducted, geared propfan intended for the Ilyushin Il-96, Tupolev Tu-204 and Tupolev Tu-330.
• NK-94 propfan. Cryogenic, liquefied natural gas (LNG) version of the NK-93.{{cite web |title=Tu-330 variants |url=https://www.globalsecurity.org/military/world/russia/tu-330-variants.htm |archive-url=https://web.archive.org/web/20150619052643/https://www.globalsecurity.org/military/world/russia/tu-330-variants.htm |url-status=live |archive-date=June 19, 2015 |website=GlobalSecurity.org |access-date=July 31, 2019}} Proposed for the 160-seat Tupolev Tu-156M2, Tu-214, and Tu-338.
• NK-104
• NK-105A
• NK-108 propfan. Like the NK-110, except in tractor instead of pusher configuration.{{cite web |language=Russian |page=48 |title=NK-110 |url=http://www.uvauga-dvig.narod.ru/nk-110.pdf |website=Ulyanovsk Higher Aviation School of Civil Aviation}}
• NK-110 propfan. Like the NK-62, this engine had four-bladed contra-rotating propellers of {{cvt|4.7|m|ftin}} in diameter, and it supported a cruise speed of Mach 0.75 at {{cvt|11000|m|ft}} altitude. The NK-110 had a takeoff thrust of {{cvt|176.5|kN|kgf lbf}} and TSFC of {{cvt|0.0193|kg/N/h|lb/lbf/h g/kN/s|order=out}}. In cruise it provided {{cvt|47.64|kN|kgf lbf}} thrust with a TSFC of {{cvt|0.0449|kg/N/h|lb/lbf/h g/kN/s|order=out}}. The engine was tested in December 1988 but was never certified because of funding problems.{{cite thesis |title=Configurazioni innovative di turbine di bassa pressione per motori aeronautici: studio preliminare aerodinamico e analisi affidabilistica |trans-title=Innovative low-pressure turbine configurations for aircraft engines: Preliminary aerodynamic study |url=https://flore.unifi.it/retrieve/handle/2158/597036/17939/Tesi_Dottorato_Turini_Moira%20ottimizzata.pdf |language=Italian |given=Moira |surname=Turini |pages=84–86 |date=December 2010 |degree=PhD |publisher=Università degli Studi di Firenze}} Intended for the Tupolev Tu-404.
• NK-112 turbofan. Cryogenic design intended to power the twin-engine Tupolev Tu-336 (a 120-seat stretched derivative of the Tu-334).{{cite book |title=Soviet aircraft industry |url=https://books.google.com/books?id=1ji5DgAAQBAJ |given=Peter G |surname=Dancey |publisher=Fonthill Media Limited |year=2015 |oclc=936209398 |isbn=978-1-78155-289-6}}
• NK-114 turbojet. Derived from the NK-93.{{cite magazine |magazine=Interavia |issn=1423-3215 |title=Russian engine industry in turmoil |given=Michael |surname=Taverna |date=June 1994 |department=Finance, Markets & Industry |pages=26–28 |location=Moscow, Russia }}
• NK-144 afterburning turbofan. Powered the early models of the Tupolev Tu-144 supersonic transport.
• NK-256 projectual engine with take-off thrust up to 200-220 kN
• NK-301

Kuznetsov industrial gas turbines include:

• NK-12ST. Derivative of the NK-12 turboprop. Serial production started in 1974. The engine is designed for gas pipelines.
• NK-14ST. (8 MW) 32 percent efficiency, pressure ratio of 9.5, turbine inlet temperature of {{cvt|1203|K|R C F}}, exhaust gas flow rate of {{cvt|37.1|kg/s|lb/s}}, fuel gas consumption of {{cvt|1900|kg/h|lb/h}}, and weight of {{cvt|3700|kg}}.
• NK-16ST. Derivative of the NK-8 turbofan. Serial production started in 1982. Used in gas compressor stations.
• NK-17ST/NK-18ST. Uprated versions of the NK-16ST gas turbine.
• NK-36ST. (25 MW) Derivative of the NK-32 turbofan. Development tests conducted in 1990.
• NK-37. (25 MW) Modification of the NK-36ST gas turbine. Designed for electric powerplants with a steam-gas plant. 36.4 percent efficiency, pressure ratio of 23.12, turbine inlet temperature of {{cvt|1420|K|R C F}}, exhaust gas flow rate of {{cvt|101.4|kg/s|lb/s}}, fuel gas consumption of {{cvt|5163|kg/h|lb/h}}, and weight of {{cvt|9840|kg}}.
• NK-38ST. (16 MW) Derivative of the NK-93 propfan. Development tests conducted in 1995. Serial production started in 1998.
• NK-39. (16 MW) Modification of the NK-38ST gas turbine. Designed for electric powerplants with a steam-gas plant. 38 percent efficiency, pressure ratio of 25.9, turbine inlet temperature of {{cvt|1476|K|R C F}}, exhaust gas flow rate of {{cvt|54.6|kg/s|lb/s}}, fuel gas consumption of {{cvt|6043|kg/h|lb/h}}, and weight of {{cvt|7200|kg}}.{{cite web |type=Report |work=Central Eurasia: Military affairs |series=JPRS Report |translator=Foreign Broadcast Information Service (FBIS) |title=Conversion: Aviation engine building industry |date=November 1992 |url=https://archive.org/details/DTIC_ADA333055/page/n64 |department=Aircraft, Missile, and Related Industries |pages=62–64 |publication-date=May 11, 1993 |volume=JPRS-UMA-93-015 |agency=Tekhnika I Vooruzheniye |oclc=831658655}}

In 1959, Sergey Korolev ordered a new design of rocket engine from the Kuznetsov Bureau for the Global Rocket 1 (GR-1) Fractional Orbital Bombardment System (FOBS){{Citation needed|date=January 2011}} intercontinental ballistic missile (ICBM), which was developed but never deployed. The result was the NK-9, one of the first staged-combustion cycle rocket engines. Kuznetsov developed the design into the NK-15 and NK-33 engines in the 1960s, and claimed them to be the highest-performance rocket engines ever built. The engines were to propel the N1 lunar rocket, which in the end was never successfully launched.Lindroos, Marcus. [http://ocw.mit.edu/courses/science-technology-and-society/sts-471j-engineering-apollo-the-moon-project-as-a-complex-system-spring-2007/readings/soviet_mand_lunr.pdf THE SOVIET MANNED LUNAR PROGRAM] MIT. Accessed: 4 October 2011. As of 2011, the aging NK-33 remains the most efficient (in terms of thrust-to-mass ratio) LOX/Kerosene rocket engine ever created.{{cite web | url =http://www.aerospaceguide.net/rocketengines/nk-33.html | title=NK-33 and NK-43 Rocket Engines | date=20 July 2016 }}

The Orbital Sciences Antares light-to-medium-lift launcher has two modified NK-33 in its first stage, a solid second stage and a hypergolic orbit stage.{{cite web |url=http://www.orbital.com/SpaceLaunch/Antares/ |title=Antares |publisher=Orbital}} The NK-33s are first imported from Russia to the United States and then modified into Aerojet AJ26s, which involves removing some harnessing, adding U.S. electronics, qualifying it for U.S. propellants, and modifying the steering system.{{cite news|url=http://spaceflightnow.com/news/n1003/15nk33/|title=Aerojet confirms Russian engine is ready for duty|date=March 15, 2010|publisher=Spaceflight Now|first=Stephen|last=Clark|accessdate=2010-03-18}}

The Antares rocket was successfully launched from NASA's Wallops Flight Facility on April 21, 2013. This marked the first successful launch of the NK-33 heritage engines built in early 1970s.{{cite web |url=https://www.npr.org/blogs/thetwo-way/2013/04/21/178289293/antares-rocket-launch-is-a-go-in-test-of-space-station-supply-vehicle |title=Antares Rocket Launch Is A Success, In Test Of Orbital Supply Vehicle |author=Bill Chappell |publisher=NPR |date=21 April 2013}}

Kuznetsov rocket engines include:

• Kuznetsov oxygen-rich stage-combustion RP1/LOX rocket engine family. Including NK-9, NK-15, NK-19, NK-21, NK-33, NK-39, NK-43. The original version was designed to power an ICBM. In the 1970s some improved versions were built for the ill-fated Soviet Lunar mission. More than 150 NK-33 engines were produced and stored in a warehouse ever since, with 36 engines having been sold to Aerojet general in the 1990s. Two NK-33 derived engines (Aerojet AJ-26) are used in the first stage of the Antares rocket developed by Orbital Sciences Corporation. The Antares rocket was successfully launched from NASA's Wallops Flight Facility on April 21, 2013. This marked the first successful launch of the NK-33 heritage engines built in the early 1970s. TsSKB-Progress also uses the stockpile NK-33 as the first-stage engine of the lightweight version of the Soyuz rocket family, the Soyuz-2-1v.{{cite web|url=http://www.russianspaceweb.com/soyuz1_lv.html|title=The Soyuz-1 rocket|last=Zak|first=Anatoly |publisher=Russian Space Web|accessdate=7 March 2010}}
• RD-107A rocket engine. Powers the boosters of the R-7 family including the Soyuz-FG and Soyuz-2.{{cite web |url=http://www.kuznetsov-motors.ru/en/product/rocket/rd-107-rd-108 |title=RD-107, RD-108 |publisher=JSC Kuznetsov |accessdate=2015-07-17 |archive-date=2015-07-21 |archive-url=https://web.archive.org/web/20150721151436/http://www.kuznetsov-motors.ru/en/product/rocket/rd-107-rd-108 |url-status=dead }}
• RD-108A rocket engine. Powers the core stage of the R-7 family including the Soyuz-FG and Soyuz-2.

• JSC Kuznetsov

{{reflist}}

• {{cite web |url=http://www.kuznetsov-motors.ru/en |title=JSC Kuznetsov}}
• {{cite AV media |url=https://www.imdb.com/title/tt0872854/ |title=The engines that came in from the cold |series=Equinox |via=Channel Four Television Corporation |publication-date=March 1, 2001 |minutes=10}}
• {{cite magazine |url=http://engine.aviaport.ru/issues/13/page26.html |title=Вклад научно-конструкторской школы Н.Д. Кузнецова в развитие отечественного двигателестроения |trans-title=The contribution of the ND Kuznetsova in the development of the domestic engine industry |given1=Evgeny |surname1=Gritsenko |given2=Vladimir |surname2=Orlov |language=Russian |publication-date=January–February 2001 |year=2001 |number=13 |magazine=Dvigatel |pages=26+}}
• {{cite web |website=Airbase |language=Russian |url=http://www.airbase.ru/alpha/rus/n/nk/ |title=SNTK im.N.D.Kuznetsova |url-status=live |archive-date=July 4, 2019 |archive-url=https://web.archive.org/web/20190704072346/http://www.airbase.ru/alpha/rus/n/nk/}}
• {{cite conference |doi=10.2514/6.1993-1981 |title=Propfan engines |conference=Joint Propulsion Conference and Exhibit |edition=29th |location=Monterey, California, USA |date=June 28–30, 1993 |given=N. D. |surname=Kuznetsov |conference-url=https://arc.aiaa.org/doi/book/10.2514/MJPC93}}
• {{citation |journal=Russian Aeronautics |title=Analysis of domestic aircraft gas turbine engine development dynamics |year=2008 |volume=51 |number=4 |pages=354–361 |doi=10.3103/S1068799808040028 |given1=V. A. |surname1=Zrelov |given2=M. E. |surname2=Prodanov |given3=A. I. |surname3=Belousov|s2cid=110659677 }}

{{Kuznetsov aeroengines}}

Category:Aircraft engine manufacturers of Russia

Category:Aircraft engine manufacturers of the Soviet Union

Category:Gas turbine manufacturers

Category:Marine engine manufacturers

Category:Space industry companies of Russia

Category:Rocket engine manufacturers of Russia

Category:Companies based in Samara, Russia

Category:Engine manufacturers of Russia

Category:Design bureaus