Military version of the H145. Includes Helionix digital avionics suite, a 4-axis autopilot, Fenestron tail rotor and Ariel 2E engines.

Overview

Data on design, manufacture and status

Design authority: Airbus Helicopters

Primary manufacturer: Airbus Helicopters

Parent type: Airbus Helicopters H145/EC145

Aircraft status: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Single main rotor

Dedicated control device: Fenestron/Shrouded tail rotor

Crew required: 1

Crew seating: Side-by-side

Landing gear: Skids

Overall Dimensions

Data on aircraft size

Overall Height: 3.95 m (13.0 ft)

Overall Length: 13.64 m (44.8 ft)

Overall Width: 11.00 m (36.1 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: Turbomeca Arriel 2E turbine

Engine manufacturer: Turbomeca

Max continuous power: 575 kW (771 hp)

Take-off / rated power: 667 kW (894 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 3700 kg (8157 lb)

Max Gross Weight (airborne): 3700 kg (8157 lb)

Max Range: 651 km (352 nm)

Max Endurance: 3.6 hrs (3.6 hrs)

Related VFS Resources

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Related Public Resources

Resources related to the H145M , provided by public sources across the internet.

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