Curtiss V-2
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
    
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
    
Wikimedia Commons has media related to Curtiss V2-3.
- Eckland, K.O. "Motors". Retrieved 27 July 2017.
 
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