Raven 1000 UL
| 1000 UL | |
|---|---|
| Type | Aircraft engine |
| National origin | United States |
| Manufacturer | Raven Redrives |
| Developed from | Suzuki G10 automotive engine |
The Raven 1000 UL is an American aircraft engine, designed and produced by Raven Redrives of El Prado, New Mexico for use in ultralight and homebuilt aircraft.[1]
Design and development
The engine is a development of the Suzuki G10 automotive engine. It is a three-cylinder in-line four-stroke, liquid-cooled, gasoline engine design, with a custom-designed belt-type reduction drive with reduction ratio of 2.11:1. It employs electronic ignition and produces 62 hp (46 kW) at 5700 rpm.[1]
Applications
Specifications (1000 UL)
Data from World Directory of Leisure Aviation 2011-12[1]
General characteristics
- Type: Three cylinder, in-line, liquid-cooled, four-stroke aircraft engine
- Bore: 74 mm (2.9 in)
- Stroke: 77 mm (3.0 in)
- Displacement: 993 cc (60.6 cu in)
- Dry weight: 67 kg (147.7 lb)
Components
- Fuel type: gasoline
- Cooling system: liquid
- Reduction gear: custom-designed belt-type reduction drive with reduction ratio of 2.11:1
Performance
- Power output: 62 hp (46 kW) at 5700 rpm
See also
- Related lists
References
External links
This article is issued from Wikipedia - version of the 8/9/2016. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.