Rolls-Royce Falcon
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The Rolls-Royce Falcon was an aero-engine developed in 1915. It was a smaller version of the Rolls-Royce Eagle; a liquid cooled V12 of 14.2 liters capacity, bore and stroke being 4x5.75 inches. Production began in September 1916 and was so successful that it continued until 1927, 2185 being built.
[edit] Specifications (Falcon)
General characteristics
- Type: 12-cylinder liquid-cooled Vee aircraft piston engine
- Bore: 4 in (102 mm)
- Stroke: 5.75 in (146 mm)
- Displacement: 867 in³ (14.2 L)
- Dry weight:
Components
- Cooling system: Liquid-cooled
Performance
- Power output:
- Specific power:
- Power-to-weight ratio:
