Product overview
The Shanghai Ruirui Aviation Equipment Technology Co., Ltd. LX30 Micro Turbojet Engine is a propulsion component with a body diameter of 132 mm and a body length of 330 mm. Its body weighs 2850 g. The engine has a maximum thrust of 295 N and a thrust-to-weight ratio of 10.5, with a maximum rotational speed of 106000 RPM.
The LX30 has a maximum fuel consumption of 980 ml/min and a specific fuel consumption of 1.59 kg/daN.h. Its starting-altitude range is 0~4000 m, while its maximum flight altitude is 8000 m. Starting altitude and maximum flight altitude are separate operating specifications. The engine's flight-speed range is Mach 0~0.8.
Specifications
| Specification | Value & conditions |
|---|---|
| Model | LX30 Micro Turbojet Engine |
| Body diameter | 132 mm |
| Body length | 330 mm |
| Body weight | 2850 g |
| Maximum thrust | 295 N |
| Thrust-to-weight ratio | 10.5 |
| Maximum fuel consumption | 980 ml/min |
| Specific fuel consumption | 1.59 kg/daN.h |
| Maximum rotational speed | 106000 RPM |
| Starting altitude | 0~4000 m |
| Maximum flight altitude | 8000 m |
| Flight speed | Mach 0~0.8 |
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