Product overview
The LX120 from Shanghai Ruirui Aviation Equipment Technology Co., Ltd. is a micro turbojet propulsion engine. Its body measures 246 mm in diameter and 584 mm in length, with a body weight of 14500 g. Maximum thrust is 1176 N, and the thrust-to-weight ratio is 8.3. The engine’s maximum rotational speed is 50500 RPM.
The LX120 has a maximum fuel consumption of 3430 ml/min and a specific fuel consumption of 1.40 kg/daN.h. Its starting-altitude range is 0–4000 m, while its maximum flight altitude is 8000 m. The flight-speed range is Mach 0–0.8, with starting altitude and maximum flight altitude specified separately.
Specifications
| Specification | Value & conditions |
|---|---|
| Manufacturer | Shanghai Ruirui Aviation Equipment Technology Co., Ltd. |
| Model and product type | LX120 Micro Turbojet Engine |
| Body diameter | 246 mm |
| Body length | 584 mm |
| Body weight | 14500 g |
| Maximum thrust | 1176 N |
| Thrust-to-weight ratio | 8.3 |
| Maximum fuel consumption | 3430 ml/min |
| Specific fuel consumption | 1.40 kg/daN.h |
| Maximum rotational speed | 50500 RPM |
| Starting altitude | 0–4000 m |
| Maximum flight altitude | 8000 m |
| Flight speed | Mach 0–0.8 |
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