SP-210 TS ROS (exhaust on top)

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SP-210 TS ROS (exhaust on top)
SKU: PP 10.210.002-1 Categories: , ,

On request

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

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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
  • Generator and Controller
  • Starter Generator and Controller

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

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