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- Armstrong_Siddeley_Python abstract "The Armstrong Siddeley Python was an early British turboprop engine designed and built by the Armstrong Siddeley company in the mid-1940s. Its main use was in the Westland Wyvern carrier-based heavy fighter. The prototypes had used the Rolls-Royce Eagle piston engine, but Pythons were used in production aircraft. In this application, the Python was rated at 4,110 eshp (equivalent shaft horsepower).".
- Armstrong_Siddeley_Python wikiPageExternalLink 9314.htm.
- Armstrong_Siddeley_Python wikiPageExternalLink 1949%20-%201399.html.
- Armstrong_Siddeley_Python wikiPageID "6081823".
- Armstrong_Siddeley_Python wikiPageRevisionID "573371488".
- Armstrong_Siddeley_Python aircon "52.5".
- Armstrong_Siddeley_Python combustion "11".
- Armstrong_Siddeley_Python compression "5.35".
- Armstrong_Siddeley_Python compressor "axial flow; 14 stages".
- Armstrong_Siddeley_Python developedFrom Armstrong_Siddeley_ASX.
- Armstrong_Siddeley_Python diameter "54.0".
- Armstrong_Siddeley_Python firstRun "April".
- Armstrong_Siddeley_Python hasPhotoCollection Armstrong_Siddeley_Python.
- Armstrong_Siddeley_Python length "123.2".
- Armstrong_Siddeley_Python lists "*List of aircraft engines".
- Armstrong_Siddeley_Python majorApplications Westland_Wyvern.
- Armstrong_Siddeley_Python manufacturer Armstrong_Siddeley.
- Armstrong_Siddeley_Python nationalOrigin "United Kingdom".
- Armstrong_Siddeley_Python power "4110".
- Armstrong_Siddeley_Python weight "1.2".
- Armstrong_Siddeley_Python ref "Flight".
- Armstrong_Siddeley_Python related "*Armstrong Siddeley ASX".
- Armstrong_Siddeley_Python specfuelcon "0.805".
- Armstrong_Siddeley_Python turbine "axial flow; two stages".
- Armstrong_Siddeley_Python type Gas_turbine.
- Armstrong_Siddeley_Python type Turboprop.
- Armstrong_Siddeley_Python weight "3450.0".
- Armstrong_Siddeley_Python subject Category:Armstrong_Siddeley_aircraft_engines.
- Armstrong_Siddeley_Python subject Category:Turboprop_engines_1940–1949.
- Armstrong_Siddeley_Python type AircraftEngine102687423.
- Armstrong_Siddeley_Python type ArmstrongSiddeleyAircraftEngines.
- Armstrong_Siddeley_Python type Artifact100021939.
- Armstrong_Siddeley_Python type Device103183080.
- Armstrong_Siddeley_Python type Engine103287733.
- Armstrong_Siddeley_Python type Instrumentality103575240.
- Armstrong_Siddeley_Python type Machine103699975.
- Armstrong_Siddeley_Python type Motor103789946.
- Armstrong_Siddeley_Python type Object100002684.
- Armstrong_Siddeley_Python type PhysicalEntity100001930.
- Armstrong_Siddeley_Python type Whole100003553.
- Armstrong_Siddeley_Python comment "The Armstrong Siddeley Python was an early British turboprop engine designed and built by the Armstrong Siddeley company in the mid-1940s. Its main use was in the Westland Wyvern carrier-based heavy fighter. The prototypes had used the Rolls-Royce Eagle piston engine, but Pythons were used in production aircraft. In this application, the Python was rated at 4,110 eshp (equivalent shaft horsepower).".
- Armstrong_Siddeley_Python label "Armstrong Siddeley Python".
- Armstrong_Siddeley_Python sameAs Armstrong_Siddeley_Python.
- Armstrong_Siddeley_Python sameAs m.0fp5_r.
- Armstrong_Siddeley_Python sameAs Q15733.
- Armstrong_Siddeley_Python sameAs Q15733.
- Armstrong_Siddeley_Python sameAs Armstrong_Siddeley_Python.
- Armstrong_Siddeley_Python wasDerivedFrom Armstrong_Siddeley_Python?oldid=573371488.
- Armstrong_Siddeley_Python isPrimaryTopicOf Armstrong_Siddeley_Python.