Heavy Fuel and Gasoline Engines for Unmanned Aerial Systems
SP-170 TS ROS Two Stroke Engine (exhaust on top) Dual cylinder UAS engine
SP-170 TS ROS Two Stroke Engine (exhaust on top)

Dual cylinder UAS engine

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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