HAWK 5
Hawk 5 five-seat gyroplane
A five-seat gyroplane with an engine-driven pre-rotation system that allows jump take-offs and runway-independent operation, whose rotor is always in autorotation for safety in the event of engine failure.
Enlarge Hawk 5 five-seat gyroplane
Specification
| Seats | 5 |
|---|---|
| Engine | Rolls-Royce 250-B17 turboprop |
| Power | 450 shp |
| Maximum gross mass | 1720 kg (3800 lb) |
| Approximate empty mass | 895 kg (1975 lb), including oil and standard avionics |
| Fuel capacity | 300 kg (670 lb) |
| Pilot, passengers and baggage with maximum fuel | 825 kg (1825 lb) |
| Cruise speed at maximum gross mass | up to 120 kt (222 km/h) |
| Maximum range, no reserve | approx. 315 nmi (580 km) |
| Rate of climb | over 1500 ft/min |
| Maximum operating altitude | 16000 ft |
| Take-off capability | Jump take-off using engine-driven rotor pre-rotation |
All data provided for information purposes; final specification is defined per contract.