Solo 2625-02
- Solo 2625-02
Retractable powerplant for open class planes (certified):
scope of delivery:
Engine unit with electric starter motor, engine mounts, exhaust system, coolant system, pulley drive with centrifugal clutch, prop stop unit.
Technical data:
| Power | ca 47 KW / 62 hp |
| max. Continuous rpm | 6500 l/min |
| Carburator | 2 Mikuni |
| Compression | 9,5 : 1 |
| Ignition | Ducati, Bosch W5 AC |
| Reduction gear | Toothed belt |
| Fuel consumption | 24,5 l/h |
| Weight | 24 kg |
| Alternator | 12 V 150 W |
| Lubricant | 1:50 Autosuper-2-stroke eng. oil |
| Propeller pillar | Carbon fibre |
| Prop (Technoflug) | 2-blade CRP |
(Kopie 1)
