The GEN 125 is a Japanese aircraft engine, designed and produced by the GEN Corporation for use in ultralight helicopters.
Contents
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).
The engine was designed specifically for the GEN H-4 helicopter, in which four of the engines are mounted to provide redundancy.
Variants
Applications
Specifications (GEN 125)
Data from World Directory of Leisure Aviation 2011-12
General characteristics
Components
Performance
References
GEN 125 Wikipedia(Text) CC BY-SA