Rotax 582, Rotax 582 aircraft engine, Rotax 582 engine specifications and technical data.

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Rotax 582 engine specifications and technical data.

Rotax 582UL model 99
Rotax 582 specifications and technical data

DESCRIPTION: Two cycle, two cylinder, rotary valve engine, oil-in-fuel lubrication or oil pump, liquid cooled, with integrated water pump
BORE: 76.0 mm (2.99 in.)
STROKE: 64.0 mm (2.52 in.)
DISPLACEMENT: 580.7 cc (35.44 cu. in.)
COMPRESSION: Theoretical: 11.5 - effective 5.75
POWER OUTPUT: 48 kw (64.4 HP SAE) at 6500 1/min
TORQUE: 75 nm (55.3 ft. lbs.) at 6,000 1/min.
MAX RPM: 6800 1/min.
DIRECTION OF ROTATION Counter- clockwise, viewed towards PTO
(Clockwise with Reduction installed)
CYLINDER: 2 light alloy cylinder with cast iron sleeves
PISTON: aluminum cast piston with 2 piston rings
PISTON/CYLINDER CLEARANCE: 0.06 mm (.0024")
CHT: Cylinder Head Temperatures
(Optional Values)
Normal: 110 C - 130 C or 230 F - 270 F
Maximum: 150 C or 300 F
Max. Difference: 10 C or 45 F
EGT: Exhaust Gas Temperatures Normal: 500 C - 620 C or 930 F - 1150 F
Maximum: 650 C or 1200 F
Max. Difference: 25 C or 45 F
Crankcase Temp. Max.: 80 C or 175 F
Cooling Liquid Temp Max.: 80 C or 175 F
IGNITION SYSTEM: Breakerless Ducati Capacitor Discharge Dual Ignition with magneto generator
GENERATOR OUTPUT: 170 Watts AC at 6000 RPM and 13.5 RMS
IGNITION TIMING: 1.96 mm or .077" (18 BTDC)
SPARK PLUG: 1.96 mm or .077" (18 BTDC)
ELECTRODE GAP: 0.5 mm (.02")
ROTARY VALVE TIMING: Opens: 130 BTDC Closes: 50 ATDC
CARBURETOR: 2 x Bing 54 36 mm Slide Valve
FUEL PUMP: Pneumatic fuel pump
FUEL: Regular or Premium Gasoline, octane number not below RON 90 (unleaded)
ENGINE LUBRICATION: Oil-in- fuel with Super two-cycle oil ASTM/CEC standard, mixing ratio
REDUCTION GEAR LUBRICATION: Gear oil API-GL5 or GL6, SAE 140 EP or 85W - 140 EP
PROPELLER SHAFT DIRECTION: Clockwise, viewed towards prop flange
STARTER: Rewind Starter Standard
STANDARD VERSION INCLUDES: Engine with carburetors w/ clamps, fuel pump, exhaust system
WEIGHT: Engine: wo/
exhaust, carb, fuel pump, radiator .lbs.......( 27.4 kg.)
2 Carburetors with flanges...........4.0 lbs.......( 1.8 kg.)
Exhaust system............................11.2 lbs.......( 5.1 kg.)
OPTIONAL EQUIPMENT: 2 air filters..............................................0.6 lbs.......( 0.3 kg.)
Double air filter.......................1.1 lbs........( 0.5 kg.)
Intake Silencer with filter...........2.4 lbs........( 1.1 kg.)
Integrated Radiator System
(#881-432) ...............................4.6 lbs........( 2.1 kg.)
Electric start kit, PTO side .......7.5 lbs........( 3.4 kg.)
Electric Start kit, MAG side .........9.9 lbs.........( 4.5 kg.)
Reduction box "B" (dry).....................17.6 lbs........(8.0 kg.)
OPTIONS:
  • Intake Silencer Kit with filter (requires jetting modifications)
  • After Muffler: Special after muffler fitted to exhaust canister (available in either weld-on type or clamp-on type)
  • Air filter: Two K&N RC 1200 or One K&N RC 2820
  • Hi gh Altitude Compensator: Automatic High Altitude adjustment of Carburetor calibration with modified Carburetor
  • Electric Start Kit: Electric start on MAG end.
  • Regulator/ Rectifier: #9103 Single phrase or #9251 three phase
  • Reduction Box: "B" box with ratios: 2.0 to 1, 2.238 to 1, or 2.58 to 1
  • Reduction Box "C" box with ratios: 2.62 to 1, 3.0 to 1, 3.4 to 1, 4.0 to 1
  • Cooling System: Twin Radiator kit #881-432 fitted on engine (not inverted)
    and gear box. 0.62 US gallon capacity.

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Rotax 582 blue head ultralight aircraft engine.

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