Product overview
Shanghai Ruirui Aviation Equipment Technology Co., Ltd.’s LX40 is a micro turbojet engine with a body diameter of 148.5 mm, a body length of 335 mm and a body weight of 3680 g. Its maximum thrust is 395 N, its thrust-to-weight ratio is 10.9, and its maximum rotational speed is 96000 RPM.
The LX40 has a maximum fuel consumption of 1300 ml/min and a specific fuel consumption of 1.58 kg/daN.h. Its starting-altitude range is 0–4000 m, with a maximum flight altitude of 8000 m and a flight-speed range of Mach 0–0.8.
Specifications
| Specification | Value & conditions |
|---|---|
| Manufacturer | Shanghai Ruirui Aviation Equipment Technology Co., Ltd. |
| Model and product type | LX40 Micro Turbojet Engine |
| Body diameter | 148.5 mm |
| Body length | 335 mm |
| Body weight | 3680 g |
| Maximum thrust | 395 N |
| Thrust-to-weight ratio | 10.9 |
| Maximum fuel consumption | 1300 ml/min |
| Specific fuel consumption | 1.58 kg/daN.h |
| Maximum rotational speed | 96000 RPM |
| Starting altitude | 0–4000 m |
| Maximum flight altitude | 8000 m |
| Flight speed | Mach 0–0.8 |
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