Armstrong Siddeley Python: Difference between revisions

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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''' wasis an early [[United Kingdom|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 [[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 eshp ([[equivalent shaft [[horsepower]] (eshp).

==Design and development==

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Lincoln B.2 ''RF403'' had two Pythons similarly installed and was used for high-altitude bombing trials at [[Woomera, South Australia]]. These trials were principally of the ballistic casings for the [[Blue Danube (nuclear weapon)|Blue Danube]] [[Nuclear weapon|atomic weapon]]: the Lincoln was the only available aircraft that could accommodate the large weapon casing, measuring 62 inches diameter x {{convert|24|ft|m}} in length. The Pythons were fitted to increase the [[Flight ceiling|height]] from which tests could be carried out. Maximum release height and speed for the first eleven tests was 275&nbsp;mph and {{convert|34,783|ft|m|abbr=on}} with a bombing error of 61&nbsp;ft.<ref>The National Archives, London, file ES 1/44 E4C Appendix 3 page 1.</ref>

==Python Engine on public display==

An Armstrong Siddeley Python is on display at the [[East Midlands Aeropark]] Castle Donington.

==Variants==

;ASP.1 (Python 1):reduction gear ratio 0.127:1

;ASP.2 (Python 2):reduction gear ratio 0.135:1

;ASP.3 (Python 3):

==Applications==

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|<!-- If you do not understand how to use this template, please ask at [[Wikipedia talk:WikiProject Aircraft]] -->

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|ref=''Flight''.<ref>[http://www.flightglobal.com/pdfarchive/view/1954/1954%20-%200979.html Flight Global Archive - 1954] www.flightglobal.com. Retrieved: 3 November 2008</ref>

|type=[[Turboprop]]

|length=123.2 in (3129313 mmcm)

|diameter=54 in (1372137 mmcm)

|weight=3,450 lb (15651,565 kg)

|compressor=axialAxial flow; 14 stages

|combustion=11 combustion chambers

|turbine=axialAxial flow; two stages

|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

|aircon=52.5 lb/s (23.8&nbsp; kg/s)

|turbinetemp=

|fuelcon=

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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 |edition= |editor1-last=Bridgman |editor1-first=Leonard |year=1947 |publisher=Sampson Low, Marston & Co |___location=London|pages=4d-5d4d–5d}}

{{refend}}