Rotax 535
| BRP-Rotax | |
|---|---|
| Image does not exist |
|
| Rotax 535 | |
| Production period: | unknown |
| Manufacturer: | BRP-Rotax |
| Working principle: | Otto |
| Motor design: | In-line engine |
| Drilling: | 72 mm |
| Hub: | 64 mm |
| Displacement: | 521.2 cm 3 |
| Mixture preparation: | Carburetor |
| Engine charging: | - |
| Cooling system: | Water cooling |
| Power: | 45 kW |
| Previous model: | none |
| Successor: | none |
The Rotax 535 is an aircraft engine from the Austrian manufacturer BRP-Rotax . It was developed for use in motor gliders . The first application for a type approval according to JAR 22 was made on June 29, 1982 and the engine was approved on April 27, 1983. The engine is no longer built and also no longer offered by Rotax.
construction
The Rotax 535 is a water-cooled two - cylinder two - stroke gasoline in-line engine with a displacement of 521.2 cm³ and a belt drive with a reduction of 3: 1. It has a double magnetic high voltage capacitor ignition from Bosch or Ducati and one or two carburetors . The engine develops an output of 60 HP (44 kW) at 7200 revolutions per minute and burns gasoline with 96 octane or AvGas 100LL. The lubrication is carried out by the oil / fuel mixture in the ratio 50: 1.
Models
- 535A
- Equipped with double diaphragm carburettors from Tillotson or Mikuni and a Mikuni DF 44 diaphragm fuel pump . The engine develops 60 hp (44 kW) at 7200 revolutions per minute. It was first registered on April 27, 1983.
- 535B
- with double diaphragm carburetor from Tillotson or Mikuni and a Mikuni DF 44 diaphragm fuel pump. The engine develops 55 hp (40 kW) at 7200 revolutions per minute. It was first registered on April 27, 1983.
- 535C
- with double diaphragm carburetor from Tillotson or Mikuni and a Mikuni DF 44 diaphragm fuel pump. The engine develops 60 hp (44 kW) at 7200 revolutions per minute. It was first registered on June 12, 1987.
use
- Glaser-Dirks DG-500M
- Roller shutter cutter LS9 (prototype)
- Schempp-Hirth Janus
- Schempp-Hirth Nimbus-4
- Schleicher ASH 25
Web links
Individual evidence
- ↑ a b c d e f Type Certificate Data Sheet Number: E.209. (pdf) European Aviation Safety Agency , February 26, 2010, accessed on January 17, 2020 .
- ^ Rotax Aircraft Engines - Product Range. BRP Rotax, accessed September 24, 2015 .
- ↑ The Glaser-Dirks DG500M. AOPA , accessed on September 24, 2015 .
