Product overview
Shanghai Ruirui Aviation Equipment Technology Co., Ltd.’s LX160 is a micro turbojet engine. Its body has a diameter of 264 mm and a length of 640 mm, with a body weight of 19500 g. The engine delivers a maximum thrust of 1550 N and has a thrust-to-weight ratio of 8.1. Its maximum rotational speed is 46000 RPM.
The LX160 has a maximum fuel consumption of 4500 ml/min and a specific fuel consumption of 1.36 kg/daN.h. Its starting altitude range is 0–4000 m, while its maximum flight altitude is 12000 m. The starting altitude range and maximum flight altitude are separate specifications. Flight speed is specified as Mach 0–0.8.
Specifications
| Specification | Value & conditions |
|---|---|
| Manufacturer | Shanghai Ruirui Aviation Equipment Technology Co., Ltd. |
| Model and product type | LX160 Micro Turbojet Engine |
| Body diameter | 264 mm |
| Body length | 640 mm |
| Body weight | 19500 g |
| Maximum thrust | 1550 N |
| Thrust-to-weight ratio | 8.1 |
| Maximum fuel consumption | 4500 ml/min |
| Specific fuel consumption | 1.36 kg/daN.h |
| Maximum rotational speed | 46000 RPM |
| Starting altitude | 0–4000 mEngine starting. |
| Maximum flight altitude | 12000 m |
| Flight speed | Mach 0–0.8 |
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