Rotax 532
| BRP-Rotax | |
|---|---|
| Image does not exist |
|
| Rotax 532 | |
| Production period: | unknown |
| Manufacturer: | BRP-Rotax |
| Working principle: | Otto |
| Motor design: | In-line engine |
| Valve control: | Rotary valves |
| Drilling: | 72 mm |
| Hub: | 64 mm |
| Displacement: | 521.2 cm 3 |
| Mixture preparation: | Carburetor |
| Engine charging: | - |
| Cooling system: | Water cooling |
| Power: | 48 kW |
| Dimensions: | 46.8 kg |
| Previous model: | none |
| Successor: | Rotax 582 |
The Rotax 532 is a water-cooled two - cylinder two - stroke in-line aircraft engine with an output of 48 kW (65 hp) and rotary valves . It was built by the Austrian company BRP-Rotax as an engine for ultralight aircraft .
construction
The Rotax 532 has a water-cooled cylinder head and water-cooled cylinders with rotary valves . One or two external coolers are used for cooling. The engine is lubricated by means of a gasoline / oil mixture in the ratio 50: 1. It also has a single flywheel magneto ignition from Bosch . It can be equipped with one or two carburettors . The fuel pressure is generated using a pneumatic fuel pump.
The propeller is a gear driven type Rotax B or C. A silenced exhaust and an air filter are installed as standard. The standard starter is a reversing starter . An electric starter is available as an option. The built-in alternator generates a voltage of twelve volts.
The Rotax 532 has now been replaced by the Rotax 582 .
use
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