SW300Pro‑K is a lightweight small‑sized kerosene‑driven micro turbojet engine designed exclusively for non‑military civilian flying equipment. Adopting a compact integrated layout, the engine optimizes the internal rotor and fuel supply system to achieve quick startup and outstanding high‑speed‑rotation stability.
All ignition parameters, throttle response and fuel‑pump limit voltage can be manually adjusted. This power unit fits medium‑size hobby aircraft models, light‑payload aerial‑survey unmanned aircraft, short‑range civilian patrol drones and small‑scale flight‑test equipment. All design purposes focus on aeromodel hobbies and civilian commercial aerial‑operation assignments.
| Specification Item | Detailed Parameter |
|---|---|
| Continuous Rated Thrust | 30 kg |
| Outer Shell Diameter | 132 mm |
| Whole‑Machine Length | 331.4 mm |
| Net Weight | 2560 g |
| Idle Operating Rotation Speed | 38000 rpm |
| Peak Working Rotation Speed | 98000 rpm |
| Standard Rated Exhaust Temperature | 750℃ |
| Maximum Safe Operating Temperature | ≤ 1000℃ |
| Permitted Peak Fuel Consumption | ≤820 g per minute |
| Compatible Fuel | Aviation kerosene |
| Lubricant Mix‑in Percentage | 3%‑5% |
| Fixed Routine Maintenance Interval | 25 working hours |
| Maximum Allowable Startup Duration | ≤30 s |
| Minimum Rated Input Voltage | ≥10 V |
The turbojet main body and matched control accessories are separately wrapped with thick shock‑absorbing foam padding. Precision electronic components are packed with anti‑static bags for protection against static damage during long‑distance land and sea transportation.
Heavy‑duty thickened corrugated cartons are used for outer‑layer packaging for collision‑resistance. A complete printed operation manual comes with every parcel. Custom‑tailored packaging schemes are supported for bulk‑order buyers.
