Hirth F-36
The Hirth F-36 is a single cylinder, two stroke, carburetted aircraft engine designed for use on ultralight aircraft, especially powered paragliders and very light ultralight trikes. The F-36 was formerly known as the Solo 210, before the design was purchased by Hirth. It is noted for its extremely light equipped weight of 28 lb (13 kg) including exhaust system, reduction drive and carburetor. Unit cost in 2009 was US$1819. The engine uses free air cooling, single capacitor discharge ignition, with a single integral pump-type carburetor. 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.
Applications:
Specifications:
Solo 210
Cycle: 2 stroke
No cylinders: 1
Bore: 70 mm
Stroke: 35 mm
Displacement: 210 cc
Cooling: air
Ignition: electronic
Reduction: Poly-v 1.75/1 – 3/1
Dimension: 260 x 320 x 210 mm
Weight: 12 kg
Max pwr: 14 hp at 6500 rpm
Fuel consumption: 350 G/hp/hr
F-36
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