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Curtiss V-2

From Wikipedia, the free encyclopedia

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

Quick Facts V-2, Type ...

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

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