EE J45 Micro turbine Jet-engine
No. | Item | Data |
1 | Maximum thrust (kg) | 45 |
2 | Maximum length (mm) | 345 |
3 | Maximum outer diameter (mm) | 160 |
4 | Specific fuel consumption (kg/daN.h) | 1.7 |
5 | Air flow (kg/s) | 0.875 |
6 | Pressor ratio | 3.6:1 |
7 | Maximum speed of revolution (r/min) |
80000 |
8 | Exhaust gas temperature (℃) | 580 |
9 | Dry weight (kg) | 4.5 |
10 |
Thrust-weight ratio (daN/kg) | 10 |