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| Turbojet 400daN |
| Engine diameter (mm) |
330 |
| Engine length (mm) |
1178 |
| Mass (kg) |
75 |
| Maximum thrust (daN) |
420 |
| Fuel consumption rate (kg/(daN·h)) |
1.1 |
| Operating altitude (m) |
0~15000 |
| Operating speed (Ma) |
0~0.95 |
| Service life (h) |
50 |
| Power generation capacity (kW) |
3 |
| Output voltage (V DC) |
28.5±3 |
| In - flight ignition harness |
0~6km
0~0.9Ma |
| In - flight ignition time (s) |
≤10 |
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All specifications are approximate. Specifications are subject to change without notice.
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