Rotax 582

The Rotax 582 is a two-stroke, two-cylinder, rotary valve engine, oil-in-fuel or oil injection pump, liquid cooled, gear reduction-drive engine commonly used on light sport aircraft and ultralight aircraft.

pecifications (Rotax 582)

pistonspecs

type=2-cylinder, 2-stroke, rotary valve, oil-in-fuel or oil-injected lubrication, dual carburetors, electronic dual ignition
bore=76 mm (2.99 in)
stroke=64 mm (2.52 in)
displacement=580.7 cm³ (35.44 cu in)
length=
diameter=
width=
height=
weight=59 kg 130 lb with electric starter, carburetors, fuel pump, air filters and reduction gear
valvetrain=
supercharger=
turbocharger=
fuelsystem=
fueltype=premium unleaded: RON 90 octane or higher leaded or unleaded or AVGAS 100 LL
oilsystem=oil-in-fuel (pre-mix) or oil injection
coolingsystem=liquid cooled
power=48 kW 64.4 HP SAE @ 6500 RPM 1-minute
specpower=
compression=11.5 (theoretical) - 5.75 effective
fuelcon=
specfuelcon=
oilcon=
power/weight=

References

* [http://www.rotax-aircraft-engines.com/ The official Rotax Aircraft Engines Website]