Armstrong Siddeley Python: Difference between revisions

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The '''Armstrong Siddeley Python''' wasis an early British [[turboprop]] engine that was designed and built by the [[Armstrong Siddeley]] company in the mid-1940s. Its main use was in the [[Westland Wyvern]], a [[carrier-based]] heavy fighter. The prototypes had used the [[Rolls-Royce Eagle (1944)|Rolls-Royce Eagle]] piston engine, but Pythons were used in production aircraft. In this application, the Python was rated at 4,110 [[equivalent shaft horsepower]] (eshp).

==Design and development==

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|fueltype=

|oilsystem=

|power=4,110 [[eshp]] (3,065 kW) at sea level at 8,000 rpm, including 1,180 lbf (535 kgf[[Kilopond|kp]]) exhaust thrust

|thrust=

|compression=5.35:1

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* {{cite book|last1=Gunston|first1=Bill|title=World encyclopaedia of aero engines : all major aircraft power plants, from the Wright brothers to the present day|date=1998|publisher=P. Stephens|___location=Sparkford, Nr Yeovil, Somerset, [England]|isbn=978-1852605971|edition=4th}}

* {{cite book |last=Gunston |first=Bill |title=World Encyclopaedia of Aero Engines |year=1989 |publisher=Patrick Stephens Limited |___location=Cambridge, England |isbn=978-1-85260-163-8 |edition=2nd}}

* {{cite book |title=Jane's all the World's Aircraft 1947 |editor1-last=Bridgman |editor1-first=Leonard |year=1947 |publisher=Sampson Low, Marston & Co |___location=London|pages=4d-5d4d–5d}}

{{refend}}