Armstrong Siddeley Jaguar
- Armstrong Siddeley Jaguar
The Armstrong Siddeley Jaguar was an aero engine developed by Armstrong Siddeley. The Jaguar was a petrol-fuelled air-cooled 14-cylinder two-row radial engine design. The Jaguar III was first used in 1923, followed in 1924 by the Jaguar IV and in 1926 by the Jaguar VI.
pecifications (Armstrong Siddeley Jaguar)
pistonspecs
ref= [Lumsden 2003, p.63-66.]
type=14 cylinder 2-row radial engine
bore=127 mm (5 in)
stroke=140 mm (5.5 in)
displacement=24.7 litres (1,512 cu in)
length=
diameter=
width=
height=
weight=354 kg (780 lb)
valvetrain=
supercharger=Yes
turbocharger=
fuelsystem=Carburetor
fueltype=
oilsystem=
coolingsystem=Air-cooled
power=300–400 hp depending on model
specpower=276 hp @ 1,450 rpm
compression=5.00:1
fuelcon= 19 gal/hr (71 l/std) @ cruise
specfuelcon=
oilcon=
power/weight=
Applications
* Armstrong Whitworth Argosy
* Armstrong Whitworth Atlas
* Armstrong Whitworth Siskin
* Fairey Flycatcher
* Gloster Grebe
* Handley Page Type W
* Vickers Vespa
ee also
Aeroenginecontent
related=
similar aircraft=
lists=
* List of aircraft engines
References
Notes
Bibliography
* Lumsden, Alec. "British Piston Engines and their Aircraft". Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN 1-85310-294-6.
External links
* [http://www.luftfahrtmuseum.com/htmi/itf/ajag4.htm Virtual aviation museum]
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