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The Klimov
Klimov
RD-33 is a turbofan jet engine for a lightweight fighter jet that is the primary engine for the Mikoyan MiG-29
Mikoyan MiG-29
and CAC/PAC JF-17 Thunder. It was developed in OKB-117 led by S. P. Izotov (now OAO Klimov) from 1968 with production starting in 1981. Previous generations of Russian supersonic fighters such as the MiG-21 and MiG-27 used turbojets, but western fighters such as the F-111 and F-4K introduced the use of afterburning turbofans in the 1960s which were more efficient. The RD-33 was the first afterburning turbofan engine produced by the Klimov
Klimov
company of Russia
Russia
in the 8,000 to 9,000 kilograms-force (78,000 to 88,000 N; 18,000 to 20,000 lbf) thrust class. It features a modular twin-shaft design with individual parts that can be replaced separately and has a good tolerance to the environment. The RD-33 is simple to maintain and retains good performance in challenging environments.[1]

Contents

1 Variants

1.1 RD-33 1.2 RD-33B/NB 1.3 RD-93 1.4 SMR-95 1.5 RD-33 series 3 1.6 RD-33MK

2 Specifications (RD-33)

2.1 General characteristics 2.2 Components 2.3 Performance

3 See also 4 References 5 External links

Variants[edit] In early 1970s the RD-33 was selected for new light fighter jet, later becoming Mikoyan MiG-29, the other option was Tumansky
Tumansky
R-67-300.[2] Years of development has built an extensive engine family. A newly designed thrust vectoring nozzle (TVN) is now available. New models of the RD-33 family include BARK digital monitoring and control systems. Repair and maintenance of RD-33 engines takes advantage of an information and diagnostics system (IDS). RD-33[edit] Baseline model developed in 1976 to power the MiG-29. RD-33B/NB[edit] A model without afterburner for various types of aircraft, such as the Il-102. RD-93[edit] A variant used to power the JF-17 (FC-1). According to JF-17.com "The most significant difference being the repositioning of the gearbox along the bottom of the engine casing." The Klimov
Klimov
poster at Zhuhai 2010 airshow gave the thrust range of the engine to be 79 kN Dry to 98 kN Wet.[3] This was designed specifically for FC-1 with increased thrust and relocated gearbox compared to base RD-33's. Although the increase of thrust decreased the service life of RD-93 to 2200 hours from RD-33's 4000 hours. According to Air Commodore Mehmood engines are solid and reliable: “We’ve flown 7,000 hours with the engine and we haven’t had any problems”, he said [4]

RD-5000B

A variant used to power the MiG Skat UCAV , 50.4 kN (11,340 lbf) dry thrust . SMR-95[edit]

SMR-95

A model for upgrading international 2nd and 3rd generation jet fighters. The accessory gearbox is repositioned below the engine, length can be varied depending on the adopted aircraft fuselage. The engine passed bench tests and flight tests on the Super Mirage F-1
Mirage F-1
and Super Cheetah D-2 aircraft of the South African Air Force and had achieved an improvement in flight performance and combat efficiency by a factor ranging from 1.2 to 3.0.[5] RD-33 series 3[edit] A revised model with a longer service life used on later or upgraded old variants of the MiG-29 such as MiG-29M
MiG-29M
and MiG-29SMT.[6][7] A pair of RD-33 series 3 engine equipped with TVN is currently undergoing flight tests as a component of the MiG-29OVT jet fighter.[8] RD-33MK[edit]

RD-33MK

The RD-33MK "Morskaya Osa" (Russian: Морская Оса: "Sea Wasp") is the latest model developed in 2001. It is intended to power the MiG-29K
MiG-29K
and MiG-29KUB shipborne fighters, however it has also been adopted for the MiG-35. The RD-33MK develops 7% higher thrust, is digitally controlled FADEC
FADEC
and smokeless unlike earlier RD-33 engines, has increased afterburner thrust to 9,000 kilograms-force (88,000 N; 20,000 lbf) and dry weight 1,145 kilograms (2,524 lb) compared to the baseline model through modern materials used on the cooled blades, although it retains the same length and maximum diameter. Incorporated is an infrared and optical signature visibility reduction systems. Service life has been increased to 4,000 hours. The RD-33MK ensures shipborne fighters unassisted take-off capability, retain performance in hot climate environment and, naturally, a boost in combat efficiency for MiG-29 fighter latest variant.[9][10] Specifications (RD-33)[edit] Data from Janes Aero Engines, Klimov
Klimov
Website General characteristics

Type: afterburning turbofan Length: 4,229 mm (166.50 in) Diameter: 1,040 mm (40.94 in) Dry weight: 1,055 kg (2,326 lb)

Components

Compressor: 2 spool axial, 4 low pressure stages, 9 high pressure stages Combustors: annular combustor Turbine: Single stage high pressure, single stage low pressure

Performance

Maximum thrust: 50.0 kN (11,230 lbf) Dry, 81.3 kN (18,285 lbf) Afterburning. Overall pressure ratio: 21:1 Bypass ratio: 0.49:1 Turbine
Turbine
inlet temperature: 1,407 °C (2,565 °F) Specific fuel consumption: 75 kg/(kN·h) (0.77 lb/(lbf·h)) dry, 188 kg/(kN·h) (1.85 lb/(lbf·h)) Thrust-to-weight ratio: 4.82:1 (dry), 7.9:1 (afterburning) Life expectancy: 4,000 hours

See also[edit]

Comparable engines

General Electric F404 Turbo-Union RB199

Related lists

List of aircraft engines

References[edit]

^ (in Russian) Klimov :: Production :: Aircraft Program :: RD-33 family Archived 2012-03-17 at the Wayback Machine. ^ MiG-29 development history on Airwar.ru ^ http://i56.tinypic.com/n3vu4x.jpg ^ Air international nr.6 december 2013 ^ (in Russian) Klimov :: Production :: Aircraft Program :: SMR-95 Archived 2007-09-16 at the Wayback Machine. ^ (in Russian) Rac Mig Archived July 6, 2007, at the Wayback Machine. ^ (in Russian) Rac Mig ^ (in Russian) Klimov :: Production :: Aircraft Program :: Trust Vertoring Nozzle Archived 2007-07-08 at the Wayback Machine. ^ (in Russian) Klimov :: Production :: Aircraft Program :: RD-33MK Archived 2007-10-12 at the Wayback Machine. ^ http://klimov.ru/f/download/press-kit/2100054687/2100054340/

External links[edit]

Wikimedia Commons has media related to Klimov
Klimov
RD-33.

Klimov
Klimov
official site page of RD-33 Turbofan
Turbofan
engine family Official site page of RD-33MK Official site page of Thrust
Thrust
vector nozzle Official site page of SMR-95 Official document: Prospective Project Developments 2007 RD-93 for JF-17 / FC-1 India to Build RD-33 under license India to make Mig 29 Engines with Russia RD-33 - history, versions, technical description (czech) RD-33 on Airwar.ru (russian)

v t e

Klimov
Klimov
aircraft engines

Piston engines

M-100 M-103 M-105 M-110 M-120 VK-106 VK-107 VK-108 VK-109 VK-110 VK-150

Turbojets

RD-45 VK-3 RD-500

Turbofans

RD-33

Turboprops and turboshafts

GTD-350 TV2-117 TV3-117 TV7-117 VK-800 VK-1500 VK-2500 VK-3000

v t e

Russian and former Soviet military designation sequences for radar, missile and rocket systems

Radar systems

Land-based

A-100 P-3 P-8 P-10 P-12 P-14 P-15 P-18 P-19 P-20 P-30 P-35 P-37 P-40 P-70 P-80 P-100 Kabina 66 Kasta 2E RSN-225 Azov SNR-75 1S91 30N6 36D6 64N6 76N6 96L6E 9S15 9S19 9S32 Duga Dnestr Dnepr Daryal Dunay Volga Don-2N Voronezh Container

Ship-borne

Airborne

N001 N002 N005 N006 N007 N008 N010 N011 N012 N014 N019 N025 N035 N036

Missiles

ICBM

BZhRK GR-1 R-7 R-9 R-16 R-26 R-36 R-36M R-46 RS-24 RS-26 RT-2 RT-2PM RT-2PM2 RT-20 RT-21 RT-23 RS-28 UR-100 UR-100MR UR-100N UR-200

IRBM

R-14 RSD-10

MRBM

R-5 R-12 RT-15 RT-25

SRBM

2K1 2K6 9K52 9K720 R-1 R-2 R-11 R-11A R-17 OTR-21 OTR-23 TR-1

SLBM

R-13 R-15 R-21 R-27 R-29 R-39 RSM-45 RSM-56

Surface-to-surface (cruise)

Burya RSS-40

Surface-to-surface (naval)

P-1 P-5 P-15 P-70 P-120 P-270 P-500 P-700 P-750 P-800 P-900 P-900A P-1000 RKV-500A RPK-2 RPK-6 RPK-7 URPK-3 URPK-4 URPK-5

Surface-to-air

2K11 Krug/SA-4 "Ganef" 2K12 Kub/SA-6 "Gainful" 2K22 Tunguska/SA-19 "Grison"/SA-N-11 (tracked gun-missile system including SA-19) Kashtan CIWS
Kashtan CIWS
(naval gun-missile system including SA-19/SA-N-11) 9K33 Osa/SA-8 "Gecko"/SA-N-4 9K31 Strela-1/SA-9 "Gaskin" 9K32 Strela-2, a.k.a. SA-7 Grail 9K34 Strela-3/SA-14 "Gremlin"/SA-N-8 9K38 Igla/SA-16 "Gimlet"/SA-18 "Grouse"/SA-24 "Grinch"/SA-N-10/SA-N-14 9K333 Verba 9K35 Strela-10/SA-13 "Gopher" 9K37 Buk/SA-11 "Gadfly"/SA-17 "Grizzly"/SA-N-7/SA-N-12 Pantsir-S1/SA-22 "Greyhound" (wheeled or tracked gun-missile system including SA-22) 9K330 Tor/SA-15 "Gauntlet"/SA-N-9 42S6 Morfey S-25 Berkut/SA-1 "Guild" S-75 Dvina/SA-2 "Guideline"/SA-N-2 S-125 Neva/Pechora/SA-3 "Goa"/SA-N-1 S-200 Angara/Vega/Dubna/SA-5 "Gammon" S-300/SA-10 "Grumble"/SA-12 "Gladiator/Giant"/SA-20 "Gargoyle"/SA-N-6 S-350 (50R6) Vityaz S-400 Triumf/SA-21 "Growler" S-500 55R6M "Triumfator-M." M-11 Shtorm/SA-N-3 "Goblet" Sosna-R

Air-to-surface

KSR-2 KSR-5 KS-1 K-10S KH-11 Kh-15 Kh-20 Kh-22 Kh-23 Kh-25 Kh-26 Kh-28 Kh-29 Kh-31 Kh-35 Kh-38 Kh-41 Kh-55 Kh-58 Kh-59 Kh-80 Kh-90 9M114V

Air-to-air

K-5 R-3 R-4 R-8 R-23 R-27 R-33 R-37 R-38 R-40 R-60 R-73 R-77 R-172

Anti-tank

3M6 9K111 9K112 9K114 9K115 9K115-2 9K121 9M14 9M15 9M17 9M113 9M117 9M119 9M120 9M123 9M133 Kornet-D Hermes

Unguided rockets

Air-launched

RP-1 RP-5 RP-6 RP-9 RP-15 RP-21 RS-82 RS-132

Rocket artillery

BM-14 BM-21 BM-24 BM-25 BM-27 BM-30 TOS-1

Engines

RD-8 RD-9 R-11 R-13 R-15 R-25 R-29 RD-33 RD-45 RD-58 RD-107 RD-117 RD-0120 RD-0124 RD-0146 RD-170 RD

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