Specifications .28F-33.29 Hirth F-36
1 specifications (f-33)
1.1 general characteristics
1.2 components
1.3 performance
specifications (f-33)
data recreational power engineering
general characteristics
type: single cylinder, two-stroke, aircraft engine
bore: 70 mm (2.8 in)
stroke: 54 mm (2.1 in)
displacement: 208 cc (12.7 cu in)
length: 275 mm (10.8 in)
width: 359 mm (14.1 in)
height: 341 mm (13.4 in)
dry weight: 28 lb (12.7 kg) reduction drive, exhaust system , recoil start
components
fuel system: 1 x integral pumper carburetor
fuel type: minimum of unleaded 93 octane auto fuel
oil system: 50:1 fuel/oil premix
cooling system: free air
reduction gear: 4 element cog belt ratios of 1.8:1, 2.0:1 or 2.5:1 available
performance
power output: 15 hp (11 kw) @ 6000 rpm
compression ratio: 10.6:1
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