Airbus H145M: Difference between revisions
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=Operators= | =Operators= | ||
*Not Fusion! [[Griffin]] | *Not Fusion! [[Griffin]] | ||
Latest revision as of 17:04, 5 October 2018
Airbus H145M | ||||
---|---|---|---|---|
Type | Helicopter | |||
Passengers | 9 or10 | |||
Crew | 1 or 2 | |||
Range | 345 nm | |||
Cruise Speed | 132 knots | |||
Fuel Capacity | Imperial Gallons ( Ibs) | |||
Takeoff Power | 2x ??? shp | |||
Rate of Climb | fpm | |||
Altitude Ceiling | ft | |||
Engine Type | Turbine | |||
Engine Quantity | 2 | |||
Engine | Turbomeca Arriel 2E | |||
Max Takeoff Weight | 8,157 Ibs | |||
(v1.02) |
Notes
- 5-cell Fuel System
- Main Rotor Diameter: 36'
- Max Range (no reserve): 345nm
- Max Endurance (no reserve): 3h 11min
- Jet A-1: 5.56 Ibs/gallon
Operators
- Not Fusion! Griffin