The Curtiss OXX was an early, dual ignition water-cooled V-8 aero engine derived from the Curtiss OX.[1]
Variants
- Curtiss OXX-2
- Curtiss OXX-3
- Curtiss OXX-5
- Curtiss OXX-6
Applications
Engines on display
Specifications (OXX-6)
General characteristics
- Type: 8-cylinder water-cooled Vee aircraft piston engine
- Bore: 4.25 in (114 mm)
- Stroke: 5 in (127 mm)
- Displacement: 567 in³ (9.3 L)
- Dry weight: 401 lb (182 kg)
Components
- Cooling system: Water-cooled
Performance
References
- ↑ American Aviation Historical Society. American Aviation Historical Society journal, Volumes 33-34.
- ↑ "Kansas Aviation Museum". Retrieved 17 April 2012.
- Molson, K. M. (1972) "The Curtiss OX-5 Engine." Journal of the American Aviation Historical Society.
- US Department of Transportation Federal Aviation Administration Type Certificate Data Sheet Curtiss OXX-6 (Group 2 - Domestic engines approved prior to 7/15/29)
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