Product overview
Shanghai Ruirui Aviation Equipment Technology Co., Ltd.’s LX50 is a micro turbojet engine with a maximum thrust of 500 N and a thrust-to-weight ratio of 10.6. Its body measures 178 mm in diameter and 379 mm in length, and its body weight is 4800 g. Maximum rotational speed is 82000 RPM.
The LX50’s maximum fuel consumption is 1500 ml/min, with a specific fuel consumption of 1.44 kg/daN.h. Its starting-altitude range is 0–4000 m, while its maximum flight altitude is 12000 m. The flight-speed range is Mach 0–0.8.
Specifications
| Specification | Value & conditions |
|---|---|
| Manufacturer | Shanghai Ruirui Aviation Equipment Technology Co., Ltd. |
| Model and product type | LX50 Micro Turbojet Engine |
| Body diameter | 178 mm |
| Body length | 379 mm |
| Body weight | 4800 g |
| Maximum thrust | 500 N |
| Thrust-to-weight ratio | 10.6 |
| Maximum fuel consumption | 1500 ml/min |
| Specific fuel consumption | 1.44 kg/daN.h |
| Maximum rotational speed | 82000 RPM |
| Starting altitude | 0–4000 m |
| Maximum flight altitude | 12000 m |
| Flight speed | Mach 0–0.8 |
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