Английская Википедия:GEN 125
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Шаблон:Short description Шаблон:Use dmy dates Шаблон:Use American English
The GEN 125 is a Japanese aircraft engine, designed and produced by the GEN Corporation for use in ultralight helicopters.[1]
Design and development
The engine is a twin cylinder two-stroke, horizontally-opposed, air-cooled, Шаблон:Convert, direct-drive, gasoline engine design. It employs capacitor discharge ignition and produces Шаблон:Convert at 8500 rpm. The engine weighs Шаблон:Convert.[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
- GEN 125
- Base model producing Шаблон:Convert[1]
- GEN 125-F
- Model producing Шаблон:Convert[1]
Applications
Specifications (GEN 125)
See also
References
External links