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| Type | 2-Cylinder Gas Engine |
|---|---|
| Capacity | 170 ccm / 10.37 cu in |
| Power | 12.6 hp / 9.3 kW @ 5250 rpm |
| Speed Range | 1500 – 10000 rpm |
| Weight | incl. ignition 10.03 lbs (4.56 kg) |
| Crankshaft | 4 ball bearings |
| Oil/Gasoline ratio | 1:50 / 2 % mix |
| Operating Voltage | 6 – 8.4 V DC |
| Bore diameter | 2.00 inch (51.00 mm) |
| Stroke | 1.60 inch (41.00 mm) |
| Torque | 18.1 Nm @ 4750 rpm |
The SP-170 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 | 170 ccm / 10.37 cu in |
| Power | 12.6 hp / 9.3 kW @ 5250 rpm |
| Speed Range | 1500 – 10000 rpm |
| Weight | incl. ignition 10.03 lbs (4.56 kg) |
| Crankshaft | 4 ball bearings |
| Oil/Gasoline ratio | 1:50 / 2 % mix |
| Operating Voltage | 6 – 8.4 V DC |
| Bore diameter | 2.00 inch (51.00 mm) |
| Stroke | 1.60 inch (41.00 mm) |
| Torque | 18.1 Nm @ 4750 rpm |
