Ka-22 Hoop
Year deployed | 1961 |
Wingspan | 28.0 m |
Main rotor diameter | 22.50 m |
Tail rotor diameter | m |
Length | 26.97 m |
Height | 10.04 m |
Weight | |
- empty | 25840 kg |
- normal take-off | 37500 |
- maximum take-off | 42500 |
Internal fuel | 6000 kg |
Engine | 2 GTE D-25VK |
Power | 2 x 4101 kW / 5619 hp |
Maximum speed | 350-356 km/h |
Cruising speed | 270-340 km/h |
Range | 1100 km |
Combat range | 780 km |
Rate of climb | 5500 m/min |
Service ceiling | 3000-3500 m |
Static ceiling | m |
Crew | 5 |
Useful load | Maximun - 16500 kg freight, normal - 5000 kg |
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