Technical Specifications
Configuration Project | Parameter |
Performance | 51 HP / 7500 rpm |
Idle Speed | 2000 rpm/min |
Maximum Takeoff Weight of UAV | 230 kg |
Maximum Power (kW/r/min) | 37 kW |
Generator Output | DC 28.5 V, 1000 W / 5500 rpm |
Applicable Propeller Specifications | 32×16, 40×18, 45×20 |
Startup Method | External Motor Starter |
Applicable Spark Plug Model | BM6A |
Displacement | 560 cm³ |
Cylinder Diameter × Stroke | 66 mm × 40 mm |
Compression Ratio | 10.5:1 |
Lubrication Mix Ratio | 30:1 |
Main Engine Weight | 17.5 kg |
Exhaust Pipe Weight | 140 g × 4 |
Igniter Weight | 190 g × 2 |
Igniter Operating Voltage | 6 V – 14.4 V |
Overall Dimension (L×W×H) | 370 × 310 × 410 mm |