Heavy Fuel and Gasoline Engines for Unmanned Aerial Systems
SP-210 TS ROS Two Stroke Engine (exhaust on top) Dual cylinder UAS engine
SP-210 TS ROS Two Stroke Engine (exhaust on top)

Dual cylinder UAS engine

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SP-210 TS ROS Two Stroke Engine (exhaust on top)

The SP-210 TS ROS (exhaust on top) comes with dual spark for redundancy and a rear output shaft for user flexibility.

This two-stroke dual cylinder engine with 210ccm is positioned in the 60~100kg UAS tier.

Current operational conditions include maritime and desert environments with thousands of hours achieved.

The following additional configurations can be offered:

  • No rear output shaft
  • Rear output shaft
  • Generator and Controller
  • Starter Generator and Controller
Type 2-Cylinder Gas Engine
Capacity 210 ccm / 12.81 cu in
Power 17.1 HP / 12.6 KW @ 6000 RPM
Speed Range 1500 – 10000 RPM
Weight incl. ignition 14.43 lbs (6.56 kg)
Crankshaft 4 ball bearings
Oil/Gasoline ratio 1:50 / 2% mix
Operating Voltage 6 – 8.4 V DC
Bore diameter 2.16 inch (55.00 mm)
Stroke 1.77 inch (45.00 mm)
Torque 22.5 Nm @ 5000 RPM
Exhaust system no additional options, Stainless steel
Generator / Starter Generator no additional options, Generator incl. Generator Controller, Starter Generator incl. Starter Generator Controller
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