Curtiss OXX
| OXX | |
|---|---|
    | |
| OXX-6 on display | |
| Type | V-8 water-cooled piston engine | 
| National origin | United States of America | 
| Manufacturer | Curtiss | 
| Developed from | Curtiss OX | 
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
- Aeromarine 39
 - Aeromarine 40
 - Burgess-Dunne
 - Curtiss Autoplane
 - Curtiss F
 - Curtiss FL
 - Curtiss JN-4
 - Curtiss MF
 - Curtiss N-9
 - Standard J-1
 
Engines on display
- The Kansas Aviation Museum has an OXX-6 on display.[2]
 
The Cradle of Aviation Museum, Garden City, NY has an OXX-2 on exhibit.
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
- Power output: 100 hp (75 kW) at 1,400 rpm
 - Compression ratio: 4.92:1
 
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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