GEN 125
Japanese aircraft engine
From Wikipedia, the free encyclopedia
The GEN 125 is a Japanese aircraft engine, designed and produced by the GEN Corporation for use in ultralight helicopters.[1]
| GEN 125 | |
|---|---|
| Type | Aircraft engine |
| National origin | Japan |
| Manufacturer | GEN Corporation |
| Major applications | GEN H-4 |
Design and development
The engine is a twin cylinder two-stroke, horizontally-opposed, air-cooled, 124 cc (7.6 cu in), direct-drive, gasoline engine design. It employs capacitor discharge ignition and produces 8 hp (6 kW) at 8500 rpm. The engine weighs 3 kg (6.6 lb).[1]
The engine was designed specifically for the GEN H-4 helicopter, in which four of the engines are mounted to provide redundancy.[1]
Variants
Applications
Specifications (GEN 125)
Data from World Directory of Leisure Aviation 2011-12[1]
General characteristics
- Type: Twin cylinder, two stroke aircraft engine
- Displacement: 124 cc (7.6 cu in)
- Dry weight: 3 kg (6.6 lb)
Components
- Fuel type: gasoline
- Cooling system: liquid or air
Performance
- Power output: 8 hp (6 kW) at 8500 rpm
See also
Related lists