199:
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.
227:"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
29:
304:
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
198:
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
252:
259:
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
305:
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.
1267:
166:
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.
187:
186:
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
1260:
131:. 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
767:
1253:
718:
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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.
37:
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1234:
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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
898:
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1006:
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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.
742:
839:
818:
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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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91:
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8:
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2114:
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1417:
978:
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815:
366:
988:
768:"RD-93MA Engine, to Power Pakistan JF-17 Block III Jets, Enters Thermal Chamber Tests"
182:
R-67-300. Years of development has built an extensive engine family. A newly designed
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1925:
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2310:
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884:
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864:
858:
Klimov :: Production :: Aircraft
Program :: Trust Vertoring Nozzle
843:
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801:
322:
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jet engine for a lightweight fighter jet and which is the primary engine for the
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In early 1970s the RD-33 was selected for new light fighter jet, later becoming
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2018:
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1120:
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1978:
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1968:
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and MiG-29KUB shipborne fighters, however it has also been adopted for the
240:
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A model without afterburner for various types of aircraft, such as the
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1187:
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75 kg/(kN·h) (0.77 lb/(lbf·h)) dry, 188.1 kg/(kN·h) (1.85 lb/(lbf·h))
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158:
The RD-33 was the first afterburning turbofan engine produced by the
692:
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2059:
2008:
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795:
Klimov :: Production :: Aircraft
Program :: SMR-95
444:
296:. The RD-33MK develops 7% higher thrust, is digitally controlled
289:
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1998:
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2195:
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1993:
1905:
1765:
1432:
719:"China, Pakistan ink pact to keep JF-17 tech away from India"
297:
144:
663:
466:
50.0 kN (11,230 lbf) dry, 81.3 kN (18,285 lbf) afterburning.
429:
2 spool axial, 4 low pressure stages, 9 high pressure stages
2632:
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1668:
1447:
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1437:
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743:"JF-17: Pakistan's pride that can compete F-16 and Mig-29"
974:
Klimov official site page of RD-33 Turbofan engine family
251:
1026:
RD-33 – history, versions, technical description (czech)
994:
Official document: Prospective
Project Developments 2007
449:
single stage high pressure, single stage low pressure
224:
155:turbofans in the 1960s which were more efficient.
243:UCAV, 50.4 kN (11,340 lbf) dry thrust.
2735:
1261:
1051:
239:A non-afterburning variant used to power the
1065:
496:1,407 °C (1,680 K; 2,565 °F)
1268:
1254:
1058:
1044:
984:Official site page of Thrust vector nozzle
384:
373:
1021:India to make Mig 29 Engines with Russia
716:
250:
717:Dasgupta, Saibal (September 21, 2015).
2736:
1249:
1039:
957:"HAL – Hindustan Aeronautics Limited"
576:
143:, but western fighters such as the
13:
1016:India to Build RD-33 under license
381:Janes Aero Engines, Klimov Website
188:information and diagnostics system
14:
2765:
967:
271:
27:
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931:
913:
891:
869:
848:
827:
806:
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16:Russian fighter aircraft engine
760:
735:
710:
677:
664:"JF-17 Engine | JF-17 Thunder"
656:
638:
620:
595:
570:
514:4.82 (dry), 7.9 (afterburning)
453:
1:
979:Official site page of RD-33MK
563:
420:
214:
72:Hindustan Aeronautics Limited
1031:RD-33 on Airwar.ru (russian)
989:Official site page of SMR-95
219:A variant used to power the
202:
7:
2749:Low-bypass turbofan engines
899:"Perspective Projects 2007"
524:
169:
10:
2770:
579:"Military engines: Russia"
494:Turbine inlet temperature:
283:
2625:
2575:
2524:
2515:
2405:
2324:
2183:
2047:
1934:
1896:
1845:
1774:
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1727:
1606:
1599:
1514:
1501:
1290:
1281:
1186:
1172:
1144:
1076:
501:Specific fuel consumption
246:
35:
26:
21:
2165:S-500/55R6M Triumfator-M
558:List of aircraft engines
231:Block III fighter jets.
193:
36:RD-33 on display at the
2744:Klimov aircraft engines
2145:S-200 Angara/Vega/Dubna
490:75.5 kg/s (166.5 lbm/s)
385:General characteristics
178:, the other option was
2754:1970s turbofan engines
2095:9K38 Igla/9K338 Igla-S
999:RD-93 for JF-17 / FC-1
510:Thrust-to-weight ratio
471:Overall pressure ratio
374:Specifications (RD-33)
256:
151:introduced the use of
909:on 27 September 2007.
821:July 6, 2007, at the
536:General Electric F404
350:CAC/PAC JF-17 Thunder
254:
223:(FC-1). According to
129:CAC/PAC JF-17 Thunder
92:CAC/PAC JF-17 Thunder
772:www.defenseworld.net
577:Karnozov, Vladimir.
404:4,229 mm (166.50 in)
2155:S-350 (50R6) Vityaz
1935:Surface-to-surface
1897:Surface-to-surface
603:"МиГ МиГ-29 (9–12)"
416:1,055 kg (2,326 lb)
410:1,040 mm (40.94 in)
2140:S-125 Neva/Pechora
1009:2021-12-28 at the
863:2007-07-08 at the
842:2007-07-06 at the
800:2007-09-16 at the
747:Times of Islamabad
723:The Times of India
530:Comparable engines
367:Dassault Mirage F1
257:
87:Major applications
2731:
2730:
2621:
2620:
2511:
2510:
1926:9M730 Burevestnik
1595:
1594:
1243:
1242:
1004:UEC site of RD-93
546:Turbo-Union RB199
439:annular combustor
113:
112:
2761:
2576:Rocket artillery
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1604:
1603:
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1287:
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1070:aircraft engines
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905:. Archived from
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883:. Archived from
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691:. Archived from
685:"Klimov picture"
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518:Life expectancy:
369:(non-production)
262:Super Mirage F-1
184:thrust vectoring
88:
56:
38:Luftwaffe Museum
31:
19:
18:
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2760:
2759:
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2734:
2733:
2732:
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2617:
2571:
2517:
2507:
2493:9M133M Kornet-M
2401:
2320:
2316:Kh-47M2 Kinzhal
2306:9M114V Shturm-V
2179:
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1936:
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1072:
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1011:Wayback Machine
970:
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937:
936:
932:
925:Rosoboronexport
919:
918:
914:
897:
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875:
874:
870:
865:Wayback Machine
854:
853:
849:
844:Wayback Machine
833:
832:
828:
823:Wayback Machine
812:
811:
807:
802:Wayback Machine
791:
790:
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689:i56.tinypic.com
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632:Rosoboronexport
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55:National origin
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5:
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2184:Air-to-surface
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2157:
2152:
2147:
2142:
2137:
2132:
2127:
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2117:
2112:
2107:
2105:9K35 Strela-10
2102:
2097:
2092:
2087:
2082:
2077:
2072:
2067:
2062:
2057:
2051:
2049:
2048:Surface-to-air
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2031:
2026:
2021:
2016:
2011:
2006:
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1996:
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1128:
1123:
1118:
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1108:
1103:
1098:
1093:
1088:
1082:
1080:
1078:Piston engines
1074:
1073:
1063:
1062:
1055:
1048:
1040:
1034:
1033:
1028:
1023:
1018:
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986:
981:
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969:
968:External links
966:
963:
962:
948:
930:
912:
890:
887:on 2007-10-12.
868:
847:
826:
805:
784:
759:
734:
709:
698:on 24 May 2018
676:
666:. 21 June 2011
655:
646:"RD-33-family"
637:
619:
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568:
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561:
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549:
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488:Air mass flow:
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176:Mikoyan MiG-29
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108:Shenyang FC-31
104:Mikoyan MiG-35
100:Mikoyan MiG-33
96:Mikoyan MiG-29
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2090:9K34 Strela-3
2088:
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2080:9K32 Strela-2
2078:
2076:
2075:9K31 Strela-1
2073:
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2065:2K22 Tunguska
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774:. 8 July 2020
773:
769:
763:
748:
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738:
724:
720:
713:
694:
690:
686:
680:
665:
659:
651:
647:
641:
633:
629:
623:
608:
607:www.airwar.ru
604:
598:
584:
583:Flight Global
580:
573:
569:
559:
556:
555:
554:
553:
552:Related lists
547:
544:
542:
539:
537:
534:
533:
532:
531:
519:
516:
513:
511:
507:
504:
502:
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324:
321:
320:
316:
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309:
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295:
291:
281:
279:
269:
267:
266:Super Cheetah
263:
253:
244:
242:
234:
233:
232:
230:
226:
222:
221:JF-17 Thunder
212:
210:
200:
191:
189:
185:
181:
177:
167:
165:
161:
156:
154:
150:
146:
142:
138:
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126:
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118:
109:
105:
101:
97:
93:
90:
85:
84:
80:
77:
76:
73:
69:
66:
64:Manufacturer
63:
62:
59:Soviet Union
58:
53:
52:
49:
46:
43:
42:
39:
34:
30:
25:
20:
2667:
2525:Air-launched
2160:S-400 Triumf
2070:Kashtan CIWS
1921:3M-54 Kalibr
1699:RS-28 Sarmat
1398:RSN-225 Azov
1179:
951:
942:
933:
924:
915:
907:the original
902:
893:
885:the original
880:
871:
855:(in Russian)
850:
834:(in Russian)
829:
813:(in Russian)
808:
792:(in Russian)
787:
776:. Retrieved
771:
762:
751:. Retrieved
749:. 2017-04-28
746:
737:
726:. Retrieved
722:
712:
700:. Retrieved
693:the original
688:
679:
668:. Retrieved
658:
649:
640:
631:
622:
610:. Retrieved
606:
597:
586:. Retrieved
582:
572:
551:
550:
529:
528:
517:
508:
499:
493:
487:
480:Bypass ratio
478:
469:
459:
443:
432:
426:
413:
407:
401:
394:afterburning
390:
378:
377:
312:Applications
307:
287:
275:
258:
238:
218:
206:
197:
173:
157:
153:afterburning
117:Klimov RD-33
116:
114:
2170:M-11 Shtorm
2130:S-25 Berkut
2125:42S6 Morfey
2100:9K333 Verba
1192:turboshafts
520:4,000 hours
454:Performance
427:Compressor:
414:Dry weight:
162:company of
2738:Categories
2325:Air-to-air
2135:S-75 Dvina
2120:Pantsir-S1
1916:3M-51 Alfa
1502:Ship-borne
1291:Land-based
1188:Turboprops
778:2021-07-27
753:2021-07-27
728:2021-07-27
702:12 January
670:2021-07-27
588:2023-06-06
564:References
541:Snecma M88
434:Combustors
421:Components
302:dry weight
215:RD-93/93MA
78:First run
2406:Anti-tank
2115:9K330 Tor
2055:2K11 Krug
1493:Container
1388:Kabina 66
1174:Turbofans
1146:Turbojets
943:klimov.ru
939:"RD-33MK"
921:"RD-33MK"
903:klimov.ru
881:klimov.ru
877:"RD-33MK"
650:klimov.ru
408:Diameter:
379:Data from
225:JF-17.com
203:RD-33B/NB
141:turbojets
2516:Unguided
2498:Kornet-D
2311:Hermes-A
2110:9K37 Buk
2085:9K33 Osa
2060:2K12 Kub
2009:RKV-500A
1899:(cruise)
1709:UR-100MR
1600:Missiles
1515:Airborne
1488:Voronezh
1393:Kasta 2E
1007:Archived
861:Archived
840:Archived
819:Archived
798:Archived
612:23 April
525:See also
460:Maximum
397:turbofan
241:MiG Skat
235:RD-5000B
180:Tumansky
170:Variants
121:turbofan
48:Turbofan
2703:RD-0146
2698:RD-0124
2693:RD-0120
2626:Engines
2518:rockets
2438:9K115-2
2175:Sosna-R
1937:(naval)
1714:UR-100N
1679:RT-2PM2
1284:systems
1235:VK-3000
1230:VK-2500
1225:VK-1500
1215:TV7-117
1210:TV3-117
1205:TV2-117
1200:GTD-350
837:Rac Mig
816:Rac Mig
628:"RD-33"
445:Turbine
402:Length:
290:MiG-29K
284:RD-33MK
278:MiG-29M
190:(IDS).
2723:RD-500
2718:RD-191
2713:RD-180
2708:RD-170
2688:RD-117
2683:RD-107
2567:RS-132
2503:Hermes
2301:Kh-101
2039:URPK-5
2034:URPK-4
2029:URPK-3
2004:P-1000
1999:P-900A
1911:RSS-40
1888:RSM-56
1883:RSM-45
1832:OTR-23
1827:OTR-21
1740:RSD-10
1719:UR-200
1704:UR-100
1674:RT-2PM
1483:Don-2N
1468:Daryal
1458:Dnestr
1403:SNR-75
1220:VK-800
1164:RD-500
1136:VK-150
1131:VK-110
1126:VK-109
1121:VK-108
1116:VK-107
1111:VK-106
1067:Klimov
462:thrust
361:SMR-95
294:MiG-35
255:SMR-95
247:SMR-95
209:Il-102
164:Russia
160:Klimov
137:MiG-23
133:MiG-21
68:Klimov
22:RD-33
2678:RD-58
2673:RD-45
2668:RD-33
2613:TOS-1
2608:BM-30
2603:BM-27
2598:BM-25
2593:BM-24
2588:BM-21
2583:BM-14
2562:RS-82
2557:RP-21
2552:RP-15
2488:9M133
2483:9M123
2478:9M120
2473:9M119
2468:9M117
2463:9M113
2443:9K121
2433:9K115
2428:9K114
2423:9K112
2418:9K111
2397:R-172
2296:Kh-90
2291:Kh-80
2286:Kh-59
2281:Kh-58
2276:Kh-55
2271:Kh-41
2266:Kh-38
2261:Kh-35
2256:Kh-31
2251:Kh-29
2246:Kh-28
2241:Kh-26
2236:Kh-25
2231:Kh-23
2226:Kh-22
2221:Kh-20
2216:Kh-15
2211:Kh-11
2206:K-10S
2196:KSR-5
2191:KSR-2
2150:S-300
2024:RPK-7
2019:RPK-6
2014:RPK-2
1994:P-900
1989:P-800
1984:P-750
1979:P-700
1974:P-500
1969:P-270
1964:P-120
1906:Burya
1817:R-11A
1797:9K720
1766:RT-15
1694:RT-23
1689:RT-21
1684:RT-20
1664:RS-26
1659:RS-24
1649:R-36M
1614:BZhRK
1478:Volga
1473:Dunay
1463:Dnepr
1433:96L6E
1383:P-100
1298:A-100
1282:Radar
1180:RD-33
1154:RD-45
1106:M-120
1101:M-110
1096:M-105
1091:M-103
1086:M-100
696:(JPG)
391:Type:
344:RD-93
317:RD-33
298:FADEC
229:JF-17
194:RD-33
145:F-111
139:used
119:is a
81:1974
44:Type
2663:R-29
2658:R-25
2653:R-15
2648:R-13
2643:R-11
2638:RD-9
2633:RD-8
2547:RP-9
2542:RP-6
2537:RP-5
2532:RP-1
2458:9M17
2453:9M15
2448:9M14
2392:R-77
2387:R-73
2382:R-60
2377:R-40
2372:R-38
2367:R-37
2362:R-33
2357:R-27
2352:R-23
2201:KS-1
1959:P-70
1954:P-15
1878:R-39
1873:R-29
1868:R-27
1863:R-21
1858:R-15
1853:R-13
1846:SLBM
1837:TR-1
1822:R-17
1812:R-11
1792:9K52
1775:SRBM
1761:R-12
1749:MRBM
1735:R-14
1728:IRBM
1669:RT-2
1654:R-46
1644:R-36
1639:R-26
1634:R-16
1619:GR-1
1607:ICBM
1587:N036
1582:N035
1577:N025
1572:N019
1567:N014
1562:N012
1557:N011
1552:N010
1547:N008
1542:N007
1537:N006
1532:N005
1527:N002
1522:N001
1453:Duga
1448:9S32
1443:9S19
1438:9S15
1428:76N6
1423:64N6
1418:36D6
1413:30N6
1408:1S91
1378:P-80
1373:P-70
1368:P-50
1363:P-40
1358:P-37
1353:P-35
1348:P-30
1343:P-20
1338:P-19
1333:P-18
1328:P-15
1323:P-14
1318:P-12
1313:P-10
1190:and
1159:VK-3
704:2022
614:2018
484:0.49
475:21:1
264:and
149:F-4K
147:and
135:and
127:and
115:The
2413:3M6
2347:R-8
2342:R-4
2337:R-3
2332:K-5
1949:P-5
1944:P-1
1807:R-2
1802:R-1
1787:2K6
1782:2K1
1756:R-5
1629:R-9
1624:R-7
1308:P-8
1303:P-3
2740::
941:.
923:.
901:.
879:.
770:.
745:.
721:.
687:.
648:.
630:.
605:.
581:.
211:.
70:/
1269:e
1262:t
1255:v
1059:e
1052:t
1045:v
959:.
945:.
927:.
781:.
756:.
731:.
706:.
673:.
652:.
634:.
616:.
591:.
512::
503::
482::
473::
464::
447::
436::
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
