Matches in DBpedia 2014 for { <http://dbpedia.org/resource/Turbomeca_Artouste> ?p ?o. }
Showing items 1 to 54 of
54
with 100 items per page.
- Turbomeca_Artouste abstract "The Turbomeca Artouste is an early French turboshaft engine, first run in 1947. Originally conceived as an auxiliary power unit (APU), it was soon adapted to aircraft propulsion, and found a niche as a powerplant for turboshaft-driven helicopters in the 1950s. Artoustes were licence-built by Bristol Siddeley (formerly Blackburn) in the UK, Hindustan Aeronautics Limited in India, and developed by Continental CAE in the USA as the Continental T51. Power is typically in the 300 kW (400 hp) range.".
- Turbomeca_Artouste wikiPageID "10208338".
- Turbomeca_Artouste wikiPageRevisionID "559542263".
- Turbomeca_Artouste combustion "Annular combustion chamber".
- Turbomeca_Artouste compressor "Single stage centrifugal".
- Turbomeca_Artouste developedInto Continental_T51.
- Turbomeca_Artouste diameter "- height, - width".
- Turbomeca_Artouste fuelcon "/hour at maximum continuous power".
- Turbomeca_Artouste fueltype "Aviation kerosene to AIR 3405".
- Turbomeca_Artouste hasPhotoCollection Turbomeca_Artouste.
- Turbomeca_Artouste lists "* List of aircraft engines".
- Turbomeca_Artouste majorApplications Aérospatiale_Alouette_II.
- Turbomeca_Artouste majorApplications "Aérospatiale Alouette III".
- Turbomeca_Artouste manufacturer Turbomeca.
- Turbomeca_Artouste nationalOrigin France.
- Turbomeca_Artouste oilsystem "Oil grade AIR 3512, pressure lubrication".
- Turbomeca_Artouste power "at 34,000 rpm for take-off".
- Turbomeca_Artouste weight "3.24".
- Turbomeca_Artouste ref "Jane's All the World's Aircraft 1962-63".
- Turbomeca_Artouste related "* Continental T51".
- Turbomeca_Artouste turbine "Three stage turbine".
- Turbomeca_Artouste type Turboshaft.
- Turbomeca_Artouste type "Turboshaft".
- Turbomeca_Artouste weight "- dry".
- Turbomeca_Artouste subject Category:Aircraft_auxiliary_power_units.
- Turbomeca_Artouste subject Category:Turbomeca_aircraft_engines.
- Turbomeca_Artouste subject Category:Turboshaft_engines_1940–1949.
- Turbomeca_Artouste type AircraftEngine102687423.
- Turbomeca_Artouste type Artifact100021939.
- Turbomeca_Artouste type Device103183080.
- Turbomeca_Artouste type Engine103287733.
- Turbomeca_Artouste type Instrumentality103575240.
- Turbomeca_Artouste type Machine103699975.
- Turbomeca_Artouste type Motor103789946.
- Turbomeca_Artouste type Object100002684.
- Turbomeca_Artouste type PhysicalEntity100001930.
- Turbomeca_Artouste type TurbomecaAircraftEngines.
- Turbomeca_Artouste type Whole100003553.
- Turbomeca_Artouste comment "The Turbomeca Artouste is an early French turboshaft engine, first run in 1947. Originally conceived as an auxiliary power unit (APU), it was soon adapted to aircraft propulsion, and found a niche as a powerplant for turboshaft-driven helicopters in the 1950s. Artoustes were licence-built by Bristol Siddeley (formerly Blackburn) in the UK, Hindustan Aeronautics Limited in India, and developed by Continental CAE in the USA as the Continental T51. Power is typically in the 300 kW (400 hp) range.".
- Turbomeca_Artouste label "Turbomeca Artouste".
- Turbomeca_Artouste label "Turbomeca Artouste".
- Turbomeca_Artouste label "Turbomeca Artouste".
- Turbomeca_Artouste label "Turbomeca Artouste".
- Turbomeca_Artouste label "チュルボメカ アルトウステ".
- Turbomeca_Artouste sameAs Turbomeca_Artouste.
- Turbomeca_Artouste sameAs Turbomeca_Artouste.
- Turbomeca_Artouste sameAs Turbomeca_Artouste.
- Turbomeca_Artouste sameAs チュルボメカ_アルトウステ.
- Turbomeca_Artouste sameAs m.02q57vr.
- Turbomeca_Artouste sameAs Q1782613.
- Turbomeca_Artouste sameAs Q1782613.
- Turbomeca_Artouste sameAs Turbomeca_Artouste.
- Turbomeca_Artouste wasDerivedFrom Turbomeca_Artouste?oldid=559542263.
- Turbomeca_Artouste isPrimaryTopicOf Turbomeca_Artouste.