V-2
Type V-8 liquid-cooled Aero-engine
National origin United States of America
Manufacturer Curtiss Aircraft
Number built 3

The Curtiss V-2 Type 3 (V-2-3) was a liquid-cooled V8 aircraft engine.

Specifications

Data from: Aerofiles Powerplants[1]

General characteristics

Components

  • Cooling system: Liquid-cooled

Performance

  • Power output: 200 hp (150 kW) at 1400 rpm

References

  1. Eckland, K.O. "Motors". Retrieved 27 July 2017.


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