SP-170 TS ROS Two Stroke Engine (exhaust on top)
The SP-170 TS ROS is a two-stroke engine with twin spark and rear output
shaft designed for a range of UAS applications.
With 170 ccm, the SP-170 TS ROS is a mid-range propulsion system designed for aircraft from 60-80kg MTOW. This engine size has completed hundreds of hours of maritime operations for EMSA in all associated operating conditions.
The SP-170 TS ROS with exhaust on top is equipped with dual spark plugs per cylinder for redundancy and a rear output shaft for user adaptability.
The following configurations can be offered:
- No rear output shaft
- Rear output shaft
- Generator and Controller
- Starter Generator and Controller
| 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 |
