Heavy Fuel and Gasoline Engines for Unmanned Aerial Systems
SP-170 FI TS ROS Two Stroke Engine Dual cylinder UAS engine
SP-170 FI TS ROS Two Stroke Engine

Dual cylinder UAS engine

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SP-170 FI TS ROS Two Stroke Engine

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

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