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







Comments

Popular posts from this blog

Memorial Series Board Lutfuddaulah Oriental Research Institute

Weak verbs Proto-Germanic grammar

History Anthrax