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| Type | 2-Cylinder Gas Engine |
|---|---|
| Capacity | 210 ccm / 12.81 cu in |
| Power | 17.1 hp / 12.6 kW @ 6000 rpm |
| Speed Range | 1500 – 10000 rpm |
| Weight | incl. ignition 14.43 lbs (6.56 kg) |
| Crankshaft | 4 ball bearings |
| Oil/Gasoline ratio | 1:50 / 2 % mix |
| Operating Voltage | 6 – 8.4 V DC |
| Bore diameter | 2.16 inch (55.00 mm) |
| Stroke | 1.77 inch (45.00 mm) |
| Torque | 22.5 Nm @ 5000 rpm |
| Exhaust system | no additional options, Stainless steel |
| Generator / Starter Generator | no additional options, Generator incl. Generator Controller, Starter Generator incl. Starter Generator Controller |
The SP-210 TS ROS is the 2-stroke engine with twin spark and rear output shaft for the most varied applications with UAV, UAS
The following additional configurations can be offered:
| Type | 2-Cylinder Gas Engine |
|---|---|
| Capacity | 210 ccm / 12.81 cu in |
| Power | 17.1 hp / 12.6 kW @ 6000 rpm |
| Speed Range | 1500 – 10000 rpm |
| Weight | incl. ignition 14.43 lbs (6.56 kg) |
| Crankshaft | 4 ball bearings |
| Oil/Gasoline ratio | 1:50 / 2 % mix |
| Operating Voltage | 6 – 8.4 V DC |
| Bore diameter | 2.16 inch (55.00 mm) |
| Stroke | 1.77 inch (45.00 mm) |
| Torque | 22.5 Nm @ 5000 rpm |
| Exhaust system | no additional options, Stainless steel |
| Generator / Starter Generator | no additional options, Generator incl. Generator Controller, Starter Generator incl. Starter Generator Controller |
