- The planning for the PL 70R2 engine goes back a few years with the first prototype test run in 2018.
- The engine is the perfect propulsion system for UAV applications.
- With the engine having 180° ignition spacing each ignition fires once on each rotation.
Benefits
The outside temperature was 27°C (80.6°F) during all tests.
Technical specifications
PL 70R2 | |
| Weight | 2740 g (6 lbs) including two ignitions |
| Power | 4.85 kW / 6.6 PS |
| Bore | 38 mm / 1.102“ |
| Stroke | 30 mm / 1.181“ |
| Speed range | 6,000 RPM |
| with 2-blade 24 x 12 carbon fiber propeller | |
| Dimensions (l x w x h) | 188 mm/7.401“ x 145 mm 5.709“ x 135 mm/5.315“ |
| Special Feature | Rear Output Shaft (ROS) is standard |
| Fuel | Two Cycle Mix 50: 1 (Gas 50/2-Cycle Oil 1) |
