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- Klimov_RD-33 abstract "The Klimov RD-33 is a turbofan engine for a lightweight fighter jet that is the primary engine for the Mikoyan MiG-29. 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 afterburnering turbofan engine produced by the Klimov company of 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.".
- Klimov_RD-33 wikiPageExternalLink 2100054340.
- Klimov_RD-33 wikiPageExternalLink 1956450.cms.
- Klimov_RD-33 wikiPageExternalLink rd33.html.
- Klimov_RD-33 wikiPageExternalLink jf-17-specifications.
- Klimov_RD-33 wikiPageExternalLink RD-33-family.
- Klimov_RD-33 wikiPageExternalLink RD-33MK.
- Klimov_RD-33 wikiPageExternalLink SMR-95.
- Klimov_RD-33 wikiPageExternalLink tvn.
- Klimov_RD-33 wikiPageExternalLink rd-33.
- Klimov_RD-33 wikiPageExternalLink 20060912.aspx.
- Klimov_RD-33 wikiPageID "4166892".
- Klimov_RD-33 wikiPageRevisionID "591224269".
- Klimov_RD-33 bypass "0.49".
- Klimov_RD-33 combustion Combustor.
- Klimov_RD-33 compression "21".
- Klimov_RD-33 compressor "2".
- Klimov_RD-33 diameter "1000.0".
- Klimov_RD-33 firstRun "1974".
- Klimov_RD-33 hasPhotoCollection Klimov_RD-33.
- Klimov_RD-33 length "4229.0".
- Klimov_RD-33 lists "*List of aircraft engines".
- Klimov_RD-33 majorApplications Mikoyan_MiG-29.
- Klimov_RD-33 majorApplications Mikoyan_MiG-35.
- Klimov_RD-33 majorApplications "JF-17 Thunder".
- Klimov_RD-33 manufacturer Klimov.
- Klimov_RD-33 ref "Janes Aero Engines, Klimov Website".
- Klimov_RD-33 similarEngines "*Eurojet EJ200 *General Electric F404 *General Electric F414 *Rolls-Royce Spey used on F-4K Phantom *TF30 used on F-111, F-14 *WS-13 *Snecma M53".
- Klimov_RD-33 specfuelcon "75".
- Klimov_RD-33 thrust "50".
- Klimov_RD-33 weight "1.44E7".
- Klimov_RD-33 turbine "Single stage high pressure, single stage low pressure".
- Klimov_RD-33 turbinetemp "1407.0".
- Klimov_RD-33 type Afterburner.
- Klimov_RD-33 type Turbofan.
- Klimov_RD-33 weight "1055.0".
- Klimov_RD-33 subject Category:Klimov_aircraft_engines.
- Klimov_RD-33 subject Category:Low-bypass_turbofan_engines.
- Klimov_RD-33 subject Category:Turbofan_engines_1970–1979.
- Klimov_RD-33 comment "The Klimov RD-33 is a turbofan engine for a lightweight fighter jet that is the primary engine for the Mikoyan MiG-29. 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.".
- Klimov_RD-33 label "Klimov RD-33".
- Klimov_RD-33 label "Klimov RD-33".
- Klimov_RD-33 label "Klimow RD-33".
- Klimov_RD-33 label "RD-33渦輪扇發動機".
- Klimov_RD-33 label "РД-33".
- Klimov_RD-33 label "كليموف أر.دي-33".
- Klimov_RD-33 label "クリーモフ RD-33".
- Klimov_RD-33 sameAs Klimov_RD-33.
- Klimov_RD-33 sameAs Klimow_RD-33.
- Klimov_RD-33 sameAs Klimov_RD-33.
- Klimov_RD-33 sameAs Klimov_RD-33.
- Klimov_RD-33 sameAs クリーモフ_RD-33.
- Klimov_RD-33 sameAs 클리모프_RD-33.
- Klimov_RD-33 sameAs m.0bmryk.
- Klimov_RD-33 sameAs Q1193142.
- Klimov_RD-33 sameAs Q1193142.
- Klimov_RD-33 wasDerivedFrom Klimov_RD-33?oldid=591224269.
- Klimov_RD-33 homepage RD-33-family.
- Klimov_RD-33 isPrimaryTopicOf Klimov_RD-33.