Английская Википедия:Hirth F-36
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The Hirth F-36 is a single-cylinder, two-stroke, carburetted aircraft engine designed for use on ultralight aircraft, especially powered paragliders and ultralight trikes. It is noted for its extremely small equipped weight of Шаблон:Convert including exhaust system, reduction drive and carburetor. It is manufactured by Hirth of Germany.[1]
The F-36 was formerly known as the Solo 210, before the design was purchased by Hirth.[2][3]
Development
The engine uses free air cooling, single capacitor discharge ignition, with a single integral pump-type carburettor. The cylinder walls are electrochemically coated with Nikasil. Standard starting is recoil start with electric start optional. A quadruple V belt reduction drive system is an option with ratios of 1.8:1, 2.0:1 or 2.5:1.[1]
The engine runs on a 50:1 pre-mix of unleaded 93 octane auto fuel and oil and produces Шаблон:Convert at 6000 rpm.[1]
Applications
Specifications (F-36)
References
External links
