Armstrong Siddeley Python: Difference between revisions

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top: Removed cost parameters - by WP:AIR consensus, these have been removed from the infobox template and will no longer display; other clean-up
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{{Use British English|date=February 2018}}
{|{{Infobox Aircraft Begin
|name= Python
|image= File:ASPython.jpg
|caption= An Armstrong Siddeley Python during [[National Advisory Committee for Aeronautics|NACA]] wind tunnel testing in 1949
}}{{Infobox Aircraft Engine
|type=[[Gas turbine]] [[turbopropTurboprop]]
|national origin= United Kingdom
|manufacturer= [[Armstrong Siddeley]]
|designer=
|first run= April {{avyear|1945}}
|introduced=
|retired=
|status=
|major applications= [[Westland Wyvern]]
|number built =
|program cost =
|unit cost =
|developed from = [[Armstrong Siddeley ASX]]
|developed into =
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|}
 
The '''Armstrong Siddeley Python''' was an early [[United Kingdom|British]] [[turboprop]] engine designed and built by the [[Armstrong Siddeley]] company in the mid-1940s. Its main use was in the [[Westland Wyvern]], a [[Aircraft carrier|carrier-based]]-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==