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The Curtiss V-2 Type 3 (V-2-3) was a liquid-cooled V8 aircraft engine.
| V-2 | |
|---|---|
| |
| Type | V-8 liquid-cooled Aero-engine |
| National origin | United States of America |
| Manufacturer | Curtiss Aircraft |
| Number built | 3 |
Specifications edit
Data from: Aerofiles Powerplants[1]
General characteristics
- Type: liquid-cooled V8 aircraft engine
- Displacement: 1,009.56 cu in (16.5437 L)
- Dry weight: 690 lb (310 kg)
Components
- Cooling system: Liquid-cooled
Performance
- Power output: 200 hp (150 kW) at 1400 rpm
References edit
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