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 an 8-cylinder Vee liquid-cooled aircraft engine.
Specifications
Data from: Aerofiles Powerplants[1]
General characteristics
- Type: 8-cylinder liquid-cooled Vee 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
- ↑ Eckland, K.O. http://aerofiles.com/motors.html. Retrieved 27 July 2017. Missing or empty
|title=
(help)
This article is issued from
Wikipedia.
The text is licensed under Creative Commons - Attribution - Sharealike.
Additional terms may apply for the media files.