About: Rolls-Royce Turbomeca Adour

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The Rolls-Royce Turbomeca Adour is a two-shaft low bypass turbofan aircraft engine developed by Rolls-Royce Turbomeca Limited, a joint venture between Rolls-Royce (UK) and Turbomeca (France). The engine is named after the Adour, a river in south western France.

Attributes	Values
rdf:type	software yago:WikicatLow-bypassTurbofanEngines yago:WikicatTurbofanEngines 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 Turbomeca Adour (cs) Rolls-Royce Turboméca Adour (de) Rolls-Royce Turbomeca Adour (fr) Rolls-Royce Turbomeca Adour (in) ロールス・ロイス・チュルボメカアドーア (ja) Rolls-Royce Turbomeca Adour (en)
rdfs:comment	Rolls-Royce Turbomeca Adour je dvouhřídelový dvouproudový letecký motor vyvinutý společností , což je společný podnik společností Rolls-Royce (Spojené království) a (Francie). Motor byl pojmenován Adour, což je řeka v jihozápadní Francii. (cs) Das Rolls-Royce Turbomeca Adour ist ein Zweiwellen-Turbofan-Triebwerk das von der Rolls-Royce Turbomeca Lmt., einer gemeinsamen Tochtergesellschaft von Rolls-Royce (Großbritannien) und Turboméca (Frankreich), entwickelt wurde. Es ist nach dem Fluss Adour im Südwesten Frankreichs benannt. (de) Le Rolls-Royce Turbomeca Adour est un turboréacteur à double flux, double corps et postcombustion développé par Rolls-Royce Turbomeca Limited, une entreprise conjointe entre le constructeur français Turbomeca et le constructeur britannique Rolls-Royce Limited. Son nom est tiré de l'Adour, un fleuve du sud-ouest de la France. (fr) The Rolls-Royce Turbomeca Adour is a two-shaft low bypass turbofan aircraft engine developed by Rolls-Royce Turbomeca Limited, a joint venture between Rolls-Royce (UK) and Turbomeca (France). The engine is named after the Adour, a river in south western France. (en) Rolls-Royce Turbomeca Adour adalah mesin pesawat turbofan dua-poros yang dikembangkan oleh Rolls-Royce Turbomeca Limited, anak perusahaan bersama Rolls-Royce (Inggris) dan Turbomeca (Prancis). Mesin ini dinamai Adour, sebuah sungai di selatan barat Prancis. (in) RT.172 アドーア（RT.172 Adour ）は、イギリスのロールス・ロイス・ホールディングスとフランスのチュルボメカの合弁会社であるロールス・ロイス・チュルボメカによって開発、生産された2軸式のターボファンエンジンである。このエンジンの名称はフランス南西部を流れるアドゥール川に由来する。 (ja)
foaf:depiction
dcterms:subject	1960s turbofan engines Low-bypass turbofan engines Rolls-Royce aircraft gas turbine engines France–United Kingdom military relations
Wikipage page ID	571541 (xsd:integer)
Wikipage revision ID	1073094252 (xsd:integer)
Link from a Wikipage to another Wikipage	Rolls-Royce Limited Rolls-Royce RB.203 Trent Rolls-Royce Spey Royal Air Force List of aircraft engines Aermacchi MB-338 Boeing 1960s turbofan engines Low-bypass turbofan engines Rolls-Royce aircraft gas turbine engines United States Navy McDonnell Douglas T-45 Goshawk SEPECAT Jaguar Mitsubishi F-1 Mitsubishi T-2 BAE Systems France–United Kingdom military relations Turbomeca Adour Aircraft engine Dassault nEUROn No. 6 Squadron RAF Royal Air Force Museum Cosford Turbofan T-45 Goshawk Japan Air Self-Defense Force Rolls-Royce Turbomeca Limited Afterburner BAE Hawk IHI Corporation RAF Coningsby Red Arrows BAE Taranis Unmanned combat air vehicle Afterburning
Link from a Wikipage to an external page	http://www.bharat-rakshak.com/IAF/aircraft/specs/560-bae-jaguar.html http://www.globalsecurity.org/military/systems/aircraft/systems/f405.htm https://web.archive.org/web/20080517030929/http:/www.raf.mod.uk/equipment/jaguar.cfm
sameAs	Rolls-Royce Turbomeca Adour Rolls-Royce Turbomeca Adour Rolls-Royce Turbomeca Adour Rolls-Royce Turbomeca Adour Rolls-Royce Turbomeca Adour Rolls-Royce Turbomeca Adour Rolls-Royce Turbomeca Adour Rolls-Royce Turbomeca Adour Rolls-Royce Turbomeca Adour Rolls-Royce Turbomeca Adour
thrust	6000 (xsd:integer)
thrust/weight	4.725000 (xsd:double)
turbine	1 (xsd:integer)
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