The SP-170 FI TS ROS is a two-stroke engine with twin spark and rear output shaft is designed for varied applications with UAS.
The two-stroke SP-170 TS ROS engine with 170 ccm is the mid range propulsion system designed for aircraft from 60-80kg MTOW.
This engine has successfully completed hundreds of hours of maritime operations for EMSA and has proven itself in all associated operating conditions.
The SP-170 TS ROS is fitted with dual spark plugs per cylinder for redundancy and a Rear Output Shaft (ROS) for user adaptability.
The following additional configurations can be offered:
- Generator and Controller
- Starter Generator and Controller
|Type||2-Cylinder Gas Engine|
|Capacity||170 ccm / 10.37 cu in|
|Power||13.60 HP / 10.0 KW @ 5500 RPM|
|Speed Range||1500 – 8000 RPM|
|Crankshaft||4 ball bearings|
|Oil/Gasoline ratio||1:50 / 2% mix|
|Bore diameter||2.00 inch (51.00 mm)|
|Stroke||1.60 inch (41.00 mm)|
|Torque||18.40 Nm @ 5000 RPM|