Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Airbus Helicopters H135M Lightweight Multirole Military Helicopter.
2 x Pratt & Whitney Canada PW206B2 turboshaft engines developing 817 horsepower each and driving four-bladed main rotor with shrouded, multi-bladed tail rotor unit.
Propulsion
162 mph
260 kph | 140 kts
Max Speed
20,013 ft
6,100 m | 4 miles
Service Ceiling
404 miles
650 km | 351 nm
Operational Range
2,150 ft/min
655 m/min
Rate-of-Climb