Airbus Helicopters (Eurocopter Group) - France
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(Showcased structural values pertain to the Eurocopter EC225 production variant)
2 x Turbomeca Makila 2A1 turboshaft engines developing 2,382 horsepower each while driving a five-bladed main rotor and four-bladed tail rotor.
(276 kph | 149 kts)
(5,900 m | 4 mi)
(860 km | 1,593 nm)
♦ MACH Regime (Sonic)
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
Values are derrived from a variety of categories related to the design, overall function, and historical influence of this aircraft in aviation history.
The overall rating takes into account over 60 individual factors related to this aircraft entry.
Rating is out of a possible 100 points.
This entry's maximum listed speed (171mph).
Graph average of 150 miles-per-hour.
Eurocopter EC225 operational range when compared to distances between major cities (in KM).
Max Altitude Visualization
The three qualities reflected above are altitude, speed, and range.
Showcasing era cross-over of this aircraft design.
Compared against Ilyushin IL-2 (military) and Cessna 172 (civilian).
Ribbon graphics not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective aerial campaigns / operations / aviation periods.