Armstrong Siddeley Ounce

{{Short description|1920s British piston aircraft engine}}

{{Use dmy dates|date=August 2017}}

{{Use British English|date=August 2017}}

{{Infobox Aircraft Begin

|name = Ounce

|image = File:Unmanned aerial target (mark II) engine RAE-O1058.jpg

|caption =

}}

{{Infobox Aircraft Engine

|type=Piston engine

|manufacturer=Armstrong Siddeley

|national origin=United Kingdom

|first run=1920

|major applications=

|number built =

|program cost =

|unit cost =

|developed from =

|developed into =

|variants with their own articles =

}}

The Armstrong Siddeley Ounce was a small two-cylinder aero engine developed by Armstrong Siddeley in 1920.Gunston 1989, p.18. The engine was originally conceived as a test piece but ran very well and was put into production for early ultralight aircraft and use in target drones. The Ounce used two cylinders from the preceding Jaguar I radial engine.

Applications

Specifications (Ounce)

{{pistonspecs

|

|ref=Lumsden.Lumsden 2003, p.66.

|type=Two cylinder, horizontally-opposed air cooled piston engine

|bore=5.0 in (127 mm)

|stroke=5.0 in (127 mm)

|displacement=196 cu in (3.2 L)

|length=20.5 in (521 mm)

|diameter=

|width=39.5 in (1003 mm)

|height=24.5 in (622 mm)

|weight= 170 lb (77 kg)

|valvetrain=Overhead valve

|supercharger=

|turbocharger=

|fuelsystem=Carburettor

|fueltype=

|oilsystem=

|coolingsystem=Air cooled

|power=45 hp (33.5 kW) at 1,500 rpm

|specpower=

|compression=5:1

|fuelcon=

|specfuelcon=

|oilcon=

|power/weight= 0.26 hp/lb (0.43 kW/kg)

}}

See also

{{aircontent

|see also=

|related=

|similar aircraft=

|lists=

|similar engines=

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References

=Notes=

{{reflist}}

=Bibliography=

{{refbegin}}

  • Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. {{ISBN|1-85260-163-9}}
  • Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. {{ISBN|1-85310-294-6}}.

{{refend}}