Configurator

Configure your propulsion unit according to your needs. Once you have completed the configuration, you can automatically forward this to us as an inquiry. We will then send you an offer with the costs and delivery conditions as well as a possible delivery date.

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SP-210 TS ROS (exhaust on top)

Additional information

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

*
SKU: PP 10.210.002-1

Description

The SP-210 TS ROS is the 2-stroke engine with twin spark and rear output shaft for the most varied applications with UAV, UAS.

The following additional configurations can be offered:

  • no rear output shaft
  • rear output shaft
  • starter generator and controller
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