About: Rolls-Royce/SNECMA M45H

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The Rolls-Royce/SNECMA M45H is an Anglo-French medium bypass ratio turbofan produced specifically for the twin-engined VFW-Fokker 614 aircraft in the early 1970s. The design was started as a collaborative effort between Bristol Siddeley and SNECMA.

Attributes	Values
rdf:type	yago:WikicatMedium-bypassTurbofanEngines yago:WikicatRolls-RoyceAircraftGasTurbineEngines yago:AircraftEngine102687423 yago:Artifact100021939 yago:Device103183080 yago:Engine103287733 yago:Fanjet103321103 yago:Instrumentality103575240 yago:JetEngine103596285 yago:Machine103699975 yago:Motor103789946 yago:Object100002684 yago:PhysicalEntity100001930 yago:Reaction-propulsionEngine104057435 yago:WikicatJetEngines yago:Whole100003553
rdfs:label	Rolls-Royce/SNECMA M45H (fr) ロールス・ロイス/スネクマ M45H (ja) Rolls-Royce/SNECMA M45H (en)
rdfs:comment	The Rolls-Royce/SNECMA M45H is an Anglo-French medium bypass ratio turbofan produced specifically for the twin-engined VFW-Fokker 614 aircraft in the early 1970s. The design was started as a collaborative effort between Bristol Siddeley and SNECMA. (en) Le Rolls-Royce/SNECMA M45H est un réacteur d'avion produit conjointement par les motoristes Rolls-Royce et SNECMA. Il a équipé essentiellement les VFW 614. * Portail de l’aéronautique (fr) ロールス・ロイス/SNECMA M45Hは1970年代にVFW-Fokker 614専用に生産された中バイパス比のターボファンエンジンである。設計はブリストル・シドレー社とスネクマ社の共同事業として開始された。 (ja)
foaf:depiction
dct:subject	Rolls-Royce aircraft gas turbine engines Medium-bypass turbofan engines 1970s turbofan engines
Wikipage page ID	3909344 (xsd:integer)
Wikipage revision ID	1101671330 (xsd:integer)
Link from a Wikipage to another Wikipage	Rolls-Royce Limited List of aircraft engines David McMurtry Rolls-Royce aircraft gas turbine engines Renishaw plc Reverse thrust United Kingdom Deutsches Museum Flugwerft Schleissheim Variable pitch fan VFW-Fokker 614 SNECMA SNECMA M45 General Electric CF34 STOL Thrust-specific fuel consumption Musée aéronautique et spatial Safran Bristol Siddeley France Medium-bypass turbofan engines Royal Air Force Museum Cosford Turbofan Axial compressor Bypass ratio 1970s turbofan engines Snecma New Scientist and Science Journal
Link from a Wikipage to an external page	https://web.archive.org/web/20160306131232/http:/www.flightglobal.com/pdfarchive/view/1971/1971%20-%200096.html
sameAs	Rolls-Royce/SNECMA M45H Rolls-Royce/SNECMA M45H Rolls-Royce/SNECMA M45H Rolls-Royce/SNECMA M45H Rolls-Royce/SNECMA M45H Rolls-Royce/SNECMA M45H Rolls-Royce/SNECMA M45H
similar engines	*General Electric CF34 (en)
thrust	7300 (xsd:integer)
thrust/weight	4.900000 (xsd:double)
turbine	3 (xsd:integer)
dbp:wikiPageUsesTemplate	dbt:Cite_magazine dbt:Commons_category dbt:Convert dbt:Cvt dbt:ISBN dbt:Reflist dbt:Short_description dbt:Use_British_English dbt:Use_dmy_dates dbt:When dbt:GBurl dbt:Cns dbt:Joint_development_aeroengines dbt:Jetspecs dbt:Aircontent dbt:Infobox_Aircraft_Engine
thumbnail	wiki-commons:Special:FilePath/Rolls_Royce_45H.jpg?width=300
national origin	United Kingdom France
diameter	909.0 (millimetre)
length	2600.0 (millimetre)
manufacturer	Rolls-Royce Limited Snecma
ref	Jane's All the World's Aircraft 1971-72. (en)
related	* SNECMA M45 (en)
type	Turbofan
weight	673.0 (kilogram)
has abstract	The Rolls-Royce/SNECMA M45H is an Anglo-French medium bypass ratio turbofan produced specifically for the twin-engined VFW-Fokker 614 aircraft in the early 1970s. The design was started as a collaborative effort between Bristol Siddeley and SNECMA. (en)

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