The Virtual Aviation Museum Armstrong Siddeley Puma (original) (raw)

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| Type sheet: apuma | | | | | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ | -------------- | ------------- | | | Armstrong Siddeley PumaWatercooled 6-cylinder inline engine, United Kingdom, 1918 [Technical Data] [Expo/Images] - [Armstrong Siddeley] [Piston Engines 1914-1918] | | | | | Features | | | | | Kind : | KRei | | | | No of cylinders : | 6 | 6 | | | 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 : | Carburetor | | | | 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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