Rotax 532 Piston Engine

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Aircraft Engine Manufacturer
Rotax
Aircraft Engine Type
Piston
Dry Weight (kg)
46.8
Wikipedia Article (URL)
en.wikipedia.org/wiki/Rotax_532
Fuel
premium unleaded: RON 90 octane or higher leaded or unleaded or AVGAS 100 LL
Oil System
oil-in-fuel (pre-mix) at 50:1
Cylinders
2
Cylinders Disposition
rotary
Bore (mm)
72
Stroke (mm)
64
Displacement (L)
0.5213
Valvetrain
rotary inlet valve, piston ported exhaust
Cooling
liquid cooled
Maximum Takeoff Power (kW)
48
Power To Weight (kW/kg)
1.019

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Family, EASA ID, Comment, Full Weight, Diameter, Max Rotating Diameter, Length, Height, Width, Control System, List Price, Program launch, FETT, First Flight, Certification, Production Start, Production End, Service End, Number Built, Modules, Time Between Overhaul, National Origin, Fuel System, Supercharger, Compression Ratio, Maximum 2min 30 Power, Maximum 30min Power, Maximum 60min Power, Maximum Continuous Power, OEI30sec Power, OEI2min Power, OEI2min 30 Power, OEI30min Power, OEI Continuous Power, Maximum Takeoff Torque, Maximum 2min 30 Torque, Maximum 30min Torque, Maximum 60min Torque, Maximum Continuous Torque, OEI30sec Torque, OEI2min Torque, OEI2min 30 Torque, OEI30min Torque, OEI Continuous Torque, Output Take Off Speed, Output Max Continuous Speed, Output Transient Speed, Output OEI2min Speed, Output OEI2min 5 Speed, Output OEI30min Speed, Output Autorotation Speed, Output Clockwise Rotation, Specific Power, Torque To Weight, Specific Fuel Consumption