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PowerJet SaM146
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==Specifications (SaM146-1S18)== [[File:PowerJet SaM146.JPG|thumb|PowerJet SaM146 at [[Paris Air Show]] 2007]] {{jetspecs |<!-- If you do not understand how to use this template, please ask at [[Wikipedia talk:WikiProject Aircraft]] --> <!-- Please include units where appropriate (main comes first, alt in parentheses). If data are missing, leave the parameter blank (do not delete it). For additional lines, end your alt units with )</li> and start a new, fully-formatted line with <li> --> |ref=<ref>Gas Turbine Engines. ''Aviation Week Aerospace 2010''. [http://www.aviationweek.com/awin/aerospace/showSpecificationPage.do?parameter=displayModelData&modelId=GT325&spec=gas_turbine_engines&manufacturer=133120&progName=PowerJet%20SaM146 (subscription required)]{{dead link|date=March 2018 |bot=InternetArchiveBot |fix-attempted=yes }}. Retrieved: 4 August 2010.</ref> - Specifications labeled with (*) are from the type certification here.<ref>{{cite web |url=http://www.easa.europa.eu/certification/type-certificates/docs/engines/EASA-TCDS-E.034_PowerJet_S.A._SaM_146_series_engines-02-23112010.pdf |title=Archived copy |access-date=2011-04-28 |url-status=dead |archive-url=https://web.archive.org/web/20110523220414/http://easa.europa.eu/certification/type-certificates/docs/engines/EASA-TCDS-E.034_PowerJet_S.A._SaM_146_series_engines-02-23112010.pdf |archive-date=2011-05-23 }}. EASA Type Certificate Data Sheet. 23 June 2010. Retrieved: 4 August 2010.</ref> |type=Twin spool, [[High-bypass turbofan]] |length={{convert|3.59|m|in|abbr=on}} |diameter={{convert|1.22|m|in|abbr=on}} |weight={{convert|2260|kg|abbr=on}} *SaM146 1S18 <ref>{{Cite web|url=https://www.safran-aircraft-engines.com/commercial-engines/regional-jets/sam146/sam146-1s18|title=SaM146 1S18|date=May 29, 2015|website=Safran Aircraft Engines}}</ref> |compressor=1 stage fan, 3-stage low pressure, 6-stage high pressure [[axial compressor|axial]] |combustion=[[Combustor#Annular type|Annular]] |turbine=1-stage high pressure, 3-stage low pressure |fueltype=[[Jet fuel|Jet A, Jet A-1]], TS-1, RP (*) |compression= 28 <ref name="auto">{{Cite web|url=https://www.powerjet.aero/sam146|title=SaM146 | PowerJet|website=www.powerjet.aero|access-date=2021-05-09|archive-date=2014-11-08|archive-url=https://web.archive.org/web/20141108141140/https://www.powerjet.aero/sam146|url-status=dead}}</ref> |oilsystem= |power= |thrust={{convert|71.6|kN|abbr=on|}} *Normal Takeoff (NTO) thrust<br/>{{convert|79.2|kN|abbr=on|}} *Automatic Power Reserve (APR) takeoff thrust SaM146 1S18<ref name="auto"/> |bypass=4.4:1 <ref name="auto"/> |aircon= |turbinetemp= |fuelcon= |specfuelcon= 0.629 lb/lbf-hr (Cruise)<ref name="auto"/> |power/weight= |thrust/weight=3.5:1 }}
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