UAV
Aksungur vs TAI Anka
Aksungur is a twin-engine growth derivative of the Anka airframe, so the two share a production line and a customer. Comparing them quantifies what the second engine buys in payload and endurance.
Specification comparison
| Specification | Aksungur | TAI Anka |
|---|---|---|
| Endurance | 40 h | 30 h |
| Ceiling | 12192 m | 9144 m |
| Max speed | 250 km/h | 217 km/h |
| MTOW | 3300 kg | 1700 kg |
| Payload | 750 kg | 350 kg |
| Hardpoints | 6 | 4 |
| Nav | GNSS/INS | GNSS/INS |
| Seeker | EO/IR + SAR/GMTI | EO/IR + LRF |
Values are reproduced exactly as recorded in the DroneZone systems database. Where a figure is absent from the public record, it is marked “Not publicly disclosed” rather than estimated.
How to read this
On the attributes both systems publish as directly comparable numbers, the recorded figures break down as follows.
- Aksungur lists 40 h endurance against TAI Anka's 30 h.
- Aksungur lists 12192 m ceiling against TAI Anka's 9144 m.
- Aksungur lists 250 km/h max speed against TAI Anka's 217 km/h.
- Aksungur lists 3300 kg mtow against TAI Anka's 1700 kg.
- Aksungur lists 750 kg payload against TAI Anka's 350 kg.
- Aksungur lists 6 hardpoints against TAI Anka's 4.
Figures as stated by manufacturers and public documentation; class-level estimates are marked as such in the entries themselves.