Polish
| Miejsce pochodzenia: | Ameryka |
|---|---|
| Nazwa handlowa: | Airbus |
| Orzecznictwo: | FAA 8130-3 |
| Numer modelu: | H145 |
| Podkreślić: | Airbus H145 Complete Aircraft,H145 Complete Aircraft Solution |
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The Airbus H145 is the latest addition to the company's family of four-ton twin-engine rotorcraft. It has quickly established itself as one of the industry's leading helicopters with its built-in mission capabilities and flexibility, especially in high-altitude and hot operating conditions.
With its compact size, small footprint and spacious and flexible cabin, the helicopter is the aircraft of choice for a wide range of civil and military missions.
| Hover ceiling OGE | 2,729 m |
|---|---|
| Hover ceiling IGE | 3,807 m |
| Recommended cruise speed | 241 km/h |
| Max range with standard fuel tanks at SL | 650 km |
| Max endurance with standard fuel tanks SL | 3 h 35 min |
| Flight envelope (temperature) | -45°C +50°C |
| Max altitude for TO and landing | 6,096 m |
| Sound level during level flight | 85.7 dB |
| D-value | 13.54 m |
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| Rotor diameter | 10.8 m |
| Internal volume (cabin and cargo compartment) | 6.03 m³ |
| Crew + passengers | 1 or 2 pilots and up to 10 pax |
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| Max takeoff weight (MTOW) | 3,800 kg |
| Max takeoff weight with external load | 3,800 kg |
| Useful load | 1,905 kg |
| Engine | 2 x Safran Helicopter - Arriel 2E |
| Standard fuel tank capacity | 723 kg |
| Takeoff power | 667 kW / 894 shp |
| Empty weight, Baseline Aircraft Definitions | 1,895 kg |
| Maximum dual cargo hook load (single hook) | 1,600 kg |
| Load (HEC class D) | 800 kg |