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SP-170 TS ROS Two Stroke Engine (exhaust on top)

SP-170 TS ROS Two Stroke Engine (exhaust on top)

Region

Germany
Germany

Category

Unmanned platforms
Unmanned platforms

The SP-170 TS ROS Two Stroke Engine (exhaust on top) is dual cylinder UAS engine. 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.
Tech Specs
Type2-Cylinder Gas Engine
Capacity170 ccm / 10.37 cu in
Power12.6 HP / 9.3 KW @ 5250 RPM
Speed Range1500 – 10000 RPM
Weightincl. ignition 10.03 lbs (4.56 kg)
Crankshaft4 ball bearings
Oil/Gasoline ratio1:50 / 2% mix
Operating Voltage6 – 8.4 V DC
Bore diameter2.00 inch (51.00 mm)
Stroke1.60 inch (41.00 mm)
Torque18.1 Nm @ 4750 RPM
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