H215M Technical Information - Helicopters - Airbus

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Introduction

Airbus’ H215M responds to military requirements for a proven cost-effective, high-performing and versatile medium-heavy utility helicopter.

Technical Description

Performance

One-engine inoperative (OEI 2 min 30 s) 1,400 kW / 1,877 shp Standard fuel tank capacity 1,567 kg Max fuel tank capacity 2,334 kg Hover ceiling IGE 2,800 m Hover ceiling OGE 1,650 m Fast cruise speed 258 km/h Max range with standard fuel tanks at SL 776 km Max range with aux fuel tank 1,165 km Max endurance with standard fuel tanks SL 4 hr, 00 min Max endurance with aux fuel tank 6 hr, 05 min

Dimensions

D-value 18.70 m Rotor diameter 15.60 m Internal volume 13.42 m3

Characteristics

Crew + troops 1 to 3 crew + 24 troops Max takeoff weight (MTOW) 9,000 kg Max takeoff weight with external load 9,350 kg Useful load 4,268 kg Max External load 4,500 kg Engine type - Safran Helicopter 2 x Makila 1A1 Turboshaft Takeoff power 1,357 kW / 1,819 shp

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