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| Turbojet 800daN |
| Engine diameter (mm) |
567 |
| Engine length (mm) |
1650 |
| Mass (kg) |
175 |
| Maximum thrust (daN) |
850 |
| Ignition start height (m) |
0~9000 |
| Fuel consumption rate (kg/(daN·h)) |
1.02 |
| Thrust-to-weight ratio |
4.3 |
| Operating altitude (m) |
0~18000 |
| Service life (h) |
200 |
| Operating speed (Ma) |
0~0.95 |
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All specifications are approximate. Specifications are subject to change without notice.
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