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Type sheet: apuma

Armstrong Siddeley Puma
Watercooled 6-cylinder inline engine, United Kingdom, 1918

[Technical Data] [Expo/Images] - [ Armstrong Siddeley] [ Piston Engines 1914-1918]


Kind :



No of cylinders :




Weight :

529.20 lbs

240.00 kg


Bore :

75 in

190 mm


Cyl. diameter :

57 in

145 mm


Engine capacity :

0.000 in3

18.800 l


Gas mixture :



Cooling :

Water cooled


Performance data

Cruise r.p.m. :

1300.00 r.p.m.

1300.00 U/min


Cruise power output :

187 hp

190 ps


Cruise fuel consumption :

14 gal/hr

52 l/std


Max. r.p.m. :

1450.00 r.p.m.

1450.00 U/min


Max. power output :

243 hp

246 ps


Short term max. r.p.m. :

1500.00 r.p.m.

1500.00 U/min


Short term max. fuel consumption :

67 gal/hr

255 l/std



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The Virtual Aviation Museum
european aviation history on the Internet
Thomas Wilberg ©

TW/01/04/06 08:52:40