Curtiss D-12
From Wikipedia, the free encyclopedia
The Curtiss D-12 was an aero engine of 18.7 litres capacity. It was a water cooled V12, producing 500 hp (370kW) and weighing 671 lb (304 kg). It was designed by Arthur Nutt and used in the Curtiss CR-3 for the 1923 Schneider Trophy race. Fairey Aviation of England was licensed to built a version called the Fairey Felix.
[edit] Specifications (Curtiss D-12)
General characteristics
- Type: 12 cylinder liquid cooled 60 degree V
- Bore: 4.5 in (114 mm)
- Stroke: 6.0 in (152 mm)
- Displacement: 1,145 cu in (18.76 liters)
- Dry weight: 671 lb (304 kg)
Components
- Cooling system: liquid
Performance
- Power output: 500 hp (370 kW) @ 2,300 rpm
