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- Klimov_VK-3 abstract "The Klimov VK-3 was the first Soviet afterburning bypass turbojet engine. Designed by S V Lyunevich at Klimov, at OKB-117 in 1949, this engine first ran in 1952, and was qualified at 5,730 kg (12,632 lb) thrust (dry) and 8,440 kg (18,607 lb) thrust (with afterburner) in 1954. The VK-3 was developed for the Mikoyan-Gurevich I-3 (I-380) and I-3U/I-5 (I-410) fighters. First flown in the I-3U in July 1956, the engine's performances was good but its reliability was poor. Even after modifications in December 1956 when newly designed compressor blades were installed, developmental problems continued, the program was ultimately canceled in January 1958. The engine was superseded by the Lyulka AL-7F, a less modern but more efficient engine.".
- Klimov_VK-3 wikiPageID "48954691".
- Klimov_VK-3 wikiPageLength "3373".
- Klimov_VK-3 wikiPageOutDegree "15".
- Klimov_VK-3 wikiPageRevisionID "697572881".
- Klimov_VK-3 wikiPageWikiLink Category:Klimov_aircraft_engines.
- Klimov_VK-3 wikiPageWikiLink Category:Low-bypass_turbofan_engines.
- Klimov_VK-3 wikiPageWikiLink Category:Turbofan_engines_1950–1959.
- Klimov_VK-3 wikiPageWikiLink General_Electric_F110.
- Klimov_VK-3 wikiPageWikiLink List_of_aircraft_engines.
- Klimov_VK-3 wikiPageWikiLink Lyulka_AL-7.
- Klimov_VK-3 wikiPageWikiLink Mikoyan-Gurevich_I-3.
- Klimov_VK-3 wikiPageWikiLink Pratt_&_Whitney_F100.
- Klimov_VK-3 wikiPageWikiLink Pratt_&_Whitney_PW1120.
- Klimov_VK-3 wikiPageWikiLink Pratt_&_Whitney_TF30.
- Klimov_VK-3 wikiPageWikiLink Saturn_AL-31.
- Klimov_VK-3 wikiPageWikiLink Shenyang_WS-10.
- Klimov_VK-3 wikiPageWikiLink Turbofan.
- Klimov_VK-3 wikiPageWikiLinkText "Klimov VK-3".
- Klimov_VK-3 wikiPageWikiLinkText "VK-3".
- Klimov_VK-3 combustion "annular combustion chamber".
- Klimov_VK-3 compressor "10".
- Klimov_VK-3 lists "* List of aircraft engines".
- Klimov_VK-3 similarEngines "* Pratt & Whitney TF30 * Pratt & Whitney F100 * Pratt & Whitney PW1120 * General Electric F110 * Saturn AL-31 * Shenyang WS-10".
- Klimov_VK-3 thrust "thrust and thrust".
- Klimov_VK-3 weight "4.56".
- Klimov_VK-3 turbine "three-stage".
- Klimov_VK-3 type "afterburning turbofan".
- Klimov_VK-3 wikiPageUsesTemplate Template:Aircontent.
- Klimov_VK-3 wikiPageUsesTemplate Template:Convert.
- Klimov_VK-3 wikiPageUsesTemplate Template:Jetspecs.
- Klimov_VK-3 wikiPageUsesTemplate Template:Klimov_aeroengines.
- Klimov_VK-3 wikiPageUsesTemplate Template:Reflist.
- Klimov_VK-3 subject Category:Klimov_aircraft_engines.
- Klimov_VK-3 subject Category:Low-bypass_turbofan_engines.
- Klimov_VK-3 subject Category:Turbofan_engines_1950–1959.
- Klimov_VK-3 hypernym Engine.
- Klimov_VK-3 type Software.
- Klimov_VK-3 comment "The Klimov VK-3 was the first Soviet afterburning bypass turbojet engine. Designed by S V Lyunevich at Klimov, at OKB-117 in 1949, this engine first ran in 1952, and was qualified at 5,730 kg (12,632 lb) thrust (dry) and 8,440 kg (18,607 lb) thrust (with afterburner) in 1954. The VK-3 was developed for the Mikoyan-Gurevich I-3 (I-380) and I-3U/I-5 (I-410) fighters. First flown in the I-3U in July 1956, the engine's performances was good but its reliability was poor.".
- Klimov_VK-3 label "Klimov VK-3".
- Klimov_VK-3 sameAs Q22137295.
- Klimov_VK-3 sameAs Q22137295.
- Klimov_VK-3 wasDerivedFrom Klimov_VK-3?oldid=697572881.
- Klimov_VK-3 isPrimaryTopicOf Klimov_VK-3.