Product overview
The LX22 Micro Turbojet Engine from Shanghai Ruirui Aviation Equipment Technology Co., Ltd. is an aircraft propulsion component with a body diameter of 120 mm and a body length of 295 mm. Body weight is 1900 g. The engine delivers a maximum thrust of 220 N, with a thrust-to-weight ratio of 11.8 and a maximum rotational speed of 117000 RPM.
The LX22 has a maximum fuel consumption of 750 ml/min and a specific fuel consumption of 1.64 kg/daN.h. Its altitude specifications distinguish engine starting from flight: the starting-altitude range is 0–4000 m, while maximum flight altitude is 8000 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 | LX22 Micro Turbojet Engine |
| Body diameter | 120 mm |
| Body length | 295 mm |
| Body weight | 1900 g |
| Maximum thrust | 220 N |
| Thrust-to-weight ratio | 11.8 |
| Maximum fuel consumption | 750 ml/min |
| Specific fuel consumption | 1.64 kg/daN.h |
| Maximum rotational speed | 117000 RPM |
| Starting altitude | 0–4000 mEngine starting. |
| Maximum flight altitude | 8000 m |
| Flight speed | Mach 0–0.8 |
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