Curtiss V-2

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.

Applications

Specifications

Data from: Aerofiles Powerplants[3]

General characteristics

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.
  1. ^ Molson, Kenneth M. (1982). Canadian Aircraft since 1909. London, UK: Putnam. p. 194. ISBN 0370300955. Retrieved 6 October 2024.
  2. ^ Bowers, Peter M. (1990). Unconventional aircraft. Blue Ridge Summit, PA: TAB Books. p. 296. ISBN 0830684506. Retrieved 6 October 2024.
  3. ^ Eckland, K.O. "Motors". Retrieved 27 July 2017.