SP-210 TS ROS 2-Stroke Engine
The SP-210 TS ROS is a 2-stroke engine with twin spark and rear output shaft suitable for a variety of UAV and UAS applications.
This 2-stroke dual cylinder SP-210 engine with 210ccm is the most popular dual in the propulsion portfolio, positioned in the 60~100kg UAS tier. Current operational conditions include maritime and desert environments with 1000s hours achieved to date. The SP-210 TS ROS comes with dual spark for redundancy and a rear output shaft for user flexibility.
The following additional configurations can be offered:
- 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 |