210:
RD-33MK models. This design had an extra controllable section after the critical cross section in the Laval type nozzle. The reason was the control of the jet blast contour at high altitude, low ambient air pressure, where the exhaust gases over expanding after the exhaust section. Right after the first few example and the first few MiG-29 prototype models, this difficult control system was removed, due to the operational altitude limit of the upcoming fighter. The first few series of the basic RD-33 version had some issue with the oil system, where a leakage caused a series of problems for the test pilots, because the oil leakage generated toxic particles in the air conditioning system. After the production line was going, these kinds of teething problems were solved. The only disadvantage was a low service life, and heavy smoke, which was fixed only in the later models.
238:"The most significant difference being the repositioning of the gearbox along the bottom of the engine casing." The Klimov poster at Zhuhai 2010 airshow gave the thrust range of the engine to be 49.4 kN to 84.4 kN wet. 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. The RD-93MA is an upgrade of the RD-93 engine. The thrust of the RD-93MA is expected to 9300 kgf compared to 8300 kgf of the RD-93, a significant bump-up in power which will help the jet to carry more armaments and fly at a higher speed. This has been specifically developed to power
40:
315:
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. Infrared and optical signature visibility reduction systems have been added. Service life has been increased to 4,000 hours. The
209:
Baseline model developed in 1976 to power the MiG-29. Development work started in 1968 at the Klimov Design Bureau, led by Sergey Isotov. The first few engines for the 9.01 MiG-29 prototype were equipped with a longer nozzle, without the double wall design, which is featured on the current RD-33 and
270:
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
1278:
263:
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RD-33MK ensures unassisted take-off capability for ship-borne fighters, retains its performance in hot climates, and thereby provides a boost in combat efficiency for the latest variant of the MiG-29 fighter.
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in the 8,000 to 9,000 kilograms-force (78 to 88 kN; 18,000 to 20,000 lbf) thrust class. It features a modular twin-shaft design with individual parts that can be replaced separately.
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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
48:
142:. 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
778:
729:
1068:
279:
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.
319:
India's
Hindustan Aeronautics Limited has obtained licensed production for RD-33MK variant in 2007 and so far has produced 140 engines till 2020.
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and smokeless unlike earlier RD-33 engines, has increased afterburner thrust to 9,000 kilograms-force (88,000 N; 20,000 lbf) and
909:
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and MiG-29SMT. A pair of RD-33 series 3 engines equipped with thrust-vectoring nozzles was used to power the MiG-29OVT jet fighter.
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850:
829:
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The RD-33MK "Morskaya Osa" (Russian: Морская Оса: "Sea Wasp") is the latest model developed in 2001. It is intended to power the
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A revised model with a longer service life used on later or upgraded old variants of the MiG-29 such as
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Russian and former Soviet military designation sequences for radar, missile and rocket systems
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779:"RD-93MA Engine, to Power Pakistan JF-17 Block III Jets, Enters Thermal Chamber Tests"
193:
R-67-300. Years of development has built an extensive engine family. A newly designed
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2014:
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869:
Klimov :: Production :: Aircraft
Program :: Trust Vertoring Nozzle
134:
jet engine for a lightweight fighter jet and which is the primary engine for the
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1999:
1964:
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In early 1970s the RD-33 was selected for new light fighter jet, later becoming
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and MiG-29KUB shipborne fighters, however it has also been adopted for the
1046:
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2019:
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58:
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A model without afterburner for various types of aircraft, such as the
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2009:
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75 kg/(kN·h) (0.77 lb/(lbf·h)) dry, 188.1 kg/(kN·h) (1.85 lb/(lbf·h))
472:
219:
174:
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The RD-33 was the first afterburning turbofan engine produced by the
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17:
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806:
Klimov :: Production :: Aircraft
Program :: SMR-95
307:. The RD-33MK develops 7% higher thrust, is digitally controlled
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730:"China, Pakistan ink pact to keep JF-17 tech away from India"
674:
477:
50.0 kN (11,230 lbf) dry, 81.3 kN (18,285 lbf) afterburning.
440:
2 spool axial, 4 low pressure stages, 9 high pressure stages
754:"JF-17: Pakistan's pride that can compete F-16 and Mig-29"
985:
Klimov official site page of RD-33 Turbofan engine family
1037:
RD-33 – history, versions, technical description (czech)
1005:
Official document: Prospective
Project Developments 2007
460:
single stage high pressure, single stage low pressure
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1945:
1907:
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1617:
1610:
1525:
1512:
1301:
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1197:
1183:
1155:
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166:turbofans in the 1960s which were more efficient.
254:UCAV, 50.4 kN (11,340 lbf) dry thrust.
1272:
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250:A non-afterburning variant used to power the
8:
507:1,407 °C (1,680 K; 2,565 °F)
2532:
1614:
1298:
1279:
1265:
1257:
1069:
1055:
1047:
995:Official site page of Thrust vector nozzle
1032:India to make Mig 29 Engines with Russia
728:Dasgupta, Saibal (September 21, 2015).
580:
29:
968:"HAL – Hindustan Aeronautics Limited"
7:
154:, but western fighters such as the
1027:India to Build RD-33 under license
392:Janes Aero Engines, Klimov Website
199:information and diagnostics system
25:
38:
27:Russian fighter aircraft engine
675:"JF-17 Engine | JF-17 Thunder"
525:4.82 (dry), 7.9 (afterburning)
1:
990:Official site page of RD-33MK
83:Hindustan Aeronautics Limited
1042:RD-33 on Airwar.ru (russian)
1000:Official site page of SMR-95
230:A variant used to power the
2760:Low-bypass turbofan engines
910:"Perspective Projects 2007"
2781:
590:"Military engines: Russia"
505:Turbine inlet temperature:
512:Specific fuel consumption
46:
37:
32:
2176:S-500/55R6M Triumfator-M
569:List of aircraft engines
242:Block III fighter jets.
47:RD-33 on display at the
2755:Klimov aircraft engines
2156:S-200 Angara/Vega/Dubna
501:75.5 kg/s (166.5 lbm/s)
396:General characteristics
189:, the other option was
2765:1970s turbofan engines
2106:9K38 Igla/9K338 Igla-S
1010:RD-93 for JF-17 / FC-1
521:Thrust-to-weight ratio
482:Overall pressure ratio
385:Specifications (RD-33)
267:
162:introduced the use of
920:on 27 September 2007.
832:July 6, 2007, at the
547:General Electric F404
361:CAC/PAC JF-17 Thunder
265:
234:(FC-1). According to
140:CAC/PAC JF-17 Thunder
103:CAC/PAC JF-17 Thunder
783:www.defenseworld.net
588:Karnozov, Vladimir.
415:4,229 mm (166.50 in)
2166:S-350 (50R6) Vityaz
1946:Surface-to-surface
1908:Surface-to-surface
614:"МиГ МиГ-29 (9–12)"
427:1,055 kg (2,326 lb)
421:1,040 mm (40.94 in)
2151:S-125 Neva/Pechora
1020:2021-12-28 at the
874:2007-07-08 at the
853:2007-07-06 at the
811:2007-09-16 at the
758:Times of Islamabad
734:The Times of India
541:Comparable engines
378:Dassault Mirage F1
268:
98:Major applications
2742:
2741:
2632:
2631:
2522:
2521:
1937:9M730 Burevestnik
1606:
1605:
1254:
1253:
1015:UEC site of RD-93
557:Turbo-Union RB199
450:annular combustor
124:
123:
16:(Redirected from
2772:
2587:Rocket artillery
2533:
1615:
1299:
1281:
1274:
1267:
1258:
1081:aircraft engines
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1048:
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916:. Archived from
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894:. Archived from
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702:. Archived from
696:"Klimov picture"
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529:Life expectancy:
380:(non-production)
273:Super Mirage F-1
195:thrust vectoring
99:
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49:Luftwaffe Museum
42:
30:
21:
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2504:9M133M Kornet-M
2412:
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2327:Kh-47M2 Kinzhal
2317:9M114V Shturm-V
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1022:Wayback Machine
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936:Rosoboronexport
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66:National origin
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2116:9K35 Strela-10
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2059:Surface-to-air
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1089:Piston engines
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979:External links
977:
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901:
898:on 2007-10-12.
879:
858:
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770:
745:
720:
709:on 24 May 2018
687:
677:. 21 June 2011
666:
657:"RD-33-family"
648:
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499:Air mass flow:
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366:Shenyang FC-31
363:
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349:Mikoyan MiG-35
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344:Mikoyan MiG-33
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339:Mikoyan MiG-29
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283:RD-33 series 3
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187:Mikoyan MiG-29
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119:Shenyang FC-31
115:Mikoyan MiG-35
111:Mikoyan MiG-33
107:Mikoyan MiG-29
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2101:9K34 Strela-3
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2091:9K32 Strela-2
2089:
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785:. 8 July 2020
784:
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658:
652:
649:
644:
640:
634:
631:
619:
618:www.airwar.ru
615:
609:
606:
595:
594:Flight Global
591:
584:
581:
574:
570:
567:
566:
565:
564:
563:Related lists
558:
555:
553:
550:
548:
545:
544:
543:
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535:
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527:
524:
522:
518:
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282:
280:
278:
277:Super Cheetah
274:
264:
257:
255:
253:
245:
244:
243:
241:
237:
233:
232:JF-17 Thunder
225:
223:
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213:
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87:
84:
80:
77:
75:Manufacturer
74:
73:
70:Soviet Union
69:
64:
63:
60:
57:
54:
53:
50:
45:
41:
36:
31:
19:
2678:
2536:Air-launched
2171:S-400 Triumf
2081:Kashtan CIWS
1932:3M-54 Kalibr
1710:RS-28 Sarmat
1409:RSN-225 Azov
1190:
962:
953:
944:
935:
926:
918:the original
913:
904:
896:the original
891:
882:
866:(in Russian)
861:
845:(in Russian)
840:
824:(in Russian)
819:
803:(in Russian)
798:
787:. Retrieved
782:
773:
762:. Retrieved
760:. 2017-04-28
757:
748:
737:. Retrieved
733:
723:
711:. Retrieved
704:the original
699:
690:
679:. Retrieved
669:
660:
651:
642:
633:
621:. Retrieved
617:
608:
597:. Retrieved
593:
583:
562:
561:
540:
539:
528:
519:
510:
504:
498:
491:Bypass ratio
489:
480:
470:
454:
443:
437:
424:
418:
412:
405:afterburning
401:
389:
388:
323:Applications
318:
298:
286:
269:
249:
229:
217:
208:
184:
168:
164:afterburning
128:Klimov RD-33
127:
125:
2181:M-11 Shtorm
2141:S-25 Berkut
2136:42S6 Morfey
2111:9K333 Verba
1203:turboshafts
531:4,000 hours
465:Performance
438:Compressor:
425:Dry weight:
173:company of
2749:Categories
2336:Air-to-air
2146:S-75 Dvina
2131:Pantsir-S1
1927:3M-51 Alfa
1513:Ship-borne
1302:Land-based
1199:Turboprops
789:2021-07-27
764:2021-07-27
739:2021-07-27
713:12 January
681:2021-07-27
599:2023-06-06
575:References
552:Snecma M88
445:Combustors
432:Components
313:dry weight
226:RD-93/93MA
89:First run
2417:Anti-tank
2126:9K330 Tor
2066:2K11 Krug
1504:Container
1399:Kabina 66
1185:Turbofans
1157:Turbojets
954:klimov.ru
950:"RD-33MK"
932:"RD-33MK"
914:klimov.ru
892:klimov.ru
888:"RD-33MK"
661:klimov.ru
419:Diameter:
390:Data from
236:JF-17.com
214:RD-33B/NB
152:turbojets
2527:Unguided
2509:Kornet-D
2322:Hermes-A
2121:9K37 Buk
2096:9K33 Osa
2071:2K12 Kub
2020:RKV-500A
1910:(cruise)
1720:UR-100MR
1611:Missiles
1526:Airborne
1499:Voronezh
1404:Kasta 2E
1018:Archived
872:Archived
851:Archived
830:Archived
809:Archived
623:23 April
536:See also
471:Maximum
408:turbofan
252:MiG Skat
246:RD-5000B
191:Tumansky
181:Variants
132:turbofan
59:Turbofan
2714:RD-0146
2709:RD-0124
2704:RD-0120
2637:Engines
2529:rockets
2449:9K115-2
2186:Sosna-R
1948:(naval)
1725:UR-100N
1690:RT-2PM2
1295:systems
1246:VK-3000
1241:VK-2500
1236:VK-1500
1226:TV7-117
1221:TV3-117
1216:TV2-117
1211:GTD-350
848:Rac Mig
827:Rac Mig
639:"RD-33"
456:Turbine
413:Length:
301:MiG-29K
295:RD-33MK
289:MiG-29M
201:(IDS).
2734:RD-500
2729:RD-191
2724:RD-180
2719:RD-170
2699:RD-117
2694:RD-107
2578:RS-132
2514:Hermes
2312:Kh-101
2050:URPK-5
2045:URPK-4
2040:URPK-3
2015:P-1000
2010:P-900A
1922:RSS-40
1899:RSM-56
1894:RSM-45
1843:OTR-23
1838:OTR-21
1751:RSD-10
1730:UR-200
1715:UR-100
1685:RT-2PM
1494:Don-2N
1479:Daryal
1469:Dnestr
1414:SNR-75
1231:VK-800
1175:RD-500
1147:VK-150
1142:VK-110
1137:VK-109
1132:VK-108
1127:VK-107
1122:VK-106
1078:Klimov
473:thrust
372:SMR-95
305:MiG-35
266:SMR-95
258:SMR-95
220:Il-102
175:Russia
171:Klimov
148:MiG-23
144:MiG-21
79:Klimov
33:RD-33
2689:RD-58
2684:RD-45
2679:RD-33
2624:TOS-1
2619:BM-30
2614:BM-27
2609:BM-25
2604:BM-24
2599:BM-21
2594:BM-14
2573:RS-82
2568:RP-21
2563:RP-15
2499:9M133
2494:9M123
2489:9M120
2484:9M119
2479:9M117
2474:9M113
2454:9K121
2444:9K115
2439:9K114
2434:9K112
2429:9K111
2408:R-172
2307:Kh-90
2302:Kh-80
2297:Kh-59
2292:Kh-58
2287:Kh-55
2282:Kh-41
2277:Kh-38
2272:Kh-35
2267:Kh-31
2262:Kh-29
2257:Kh-28
2252:Kh-26
2247:Kh-25
2242:Kh-23
2237:Kh-22
2232:Kh-20
2227:Kh-15
2222:Kh-11
2217:K-10S
2207:KSR-5
2202:KSR-2
2161:S-300
2035:RPK-7
2030:RPK-6
2025:RPK-2
2005:P-900
2000:P-800
1995:P-750
1990:P-700
1985:P-500
1980:P-270
1975:P-120
1917:Burya
1828:R-11A
1808:9K720
1777:RT-15
1705:RT-23
1700:RT-21
1695:RT-20
1675:RS-26
1670:RS-24
1660:R-36M
1625:BZhRK
1489:Volga
1484:Dunay
1474:Dnepr
1444:96L6E
1394:P-100
1309:A-100
1293:Radar
1191:RD-33
1165:RD-45
1117:M-120
1112:M-110
1107:M-105
1102:M-103
1097:M-100
707:(JPG)
402:Type:
355:RD-93
328:RD-33
309:FADEC
240:JF-17
205:RD-33
156:F-111
150:used
130:is a
92:1974
55:Type
18:RD-33
2674:R-29
2669:R-25
2664:R-15
2659:R-13
2654:R-11
2649:RD-9
2644:RD-8
2558:RP-9
2553:RP-6
2548:RP-5
2543:RP-1
2469:9M17
2464:9M15
2459:9M14
2403:R-77
2398:R-73
2393:R-60
2388:R-40
2383:R-38
2378:R-37
2373:R-33
2368:R-27
2363:R-23
2212:KS-1
1970:P-70
1965:P-15
1889:R-39
1884:R-29
1879:R-27
1874:R-21
1869:R-15
1864:R-13
1857:SLBM
1848:TR-1
1833:R-17
1823:R-11
1803:9K52
1786:SRBM
1772:R-12
1760:MRBM
1746:R-14
1739:IRBM
1680:RT-2
1665:R-46
1655:R-36
1650:R-26
1645:R-16
1630:GR-1
1618:ICBM
1598:N036
1593:N035
1588:N025
1583:N019
1578:N014
1573:N012
1568:N011
1563:N010
1558:N008
1553:N007
1548:N006
1543:N005
1538:N002
1533:N001
1464:Duga
1459:9S32
1454:9S19
1449:9S15
1439:76N6
1434:64N6
1429:36D6
1424:30N6
1419:1S91
1389:P-80
1384:P-70
1379:P-50
1374:P-40
1369:P-37
1364:P-35
1359:P-30
1354:P-20
1349:P-19
1344:P-18
1339:P-15
1334:P-14
1329:P-12
1324:P-10
1201:and
1170:VK-3
715:2022
625:2018
495:0.49
486:21:1
275:and
160:F-4K
158:and
146:and
138:and
126:The
2424:3M6
2358:R-8
2353:R-4
2348:R-3
2343:K-5
1960:P-5
1955:P-1
1818:R-2
1813:R-1
1798:2K6
1793:2K1
1767:R-5
1640:R-9
1635:R-7
1319:P-8
1314:P-3
2751::
952:.
934:.
912:.
890:.
781:.
756:.
732:.
698:.
659:.
641:.
616:.
592:.
222:.
81:/
1280:e
1273:t
1266:v
1070:e
1063:t
1056:v
970:.
956:.
938:.
792:.
767:.
742:.
717:.
684:.
663:.
645:.
627:.
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