Mil Mi-17 (Hip-H) vs Airbus Helicopters H725/EC725 (Caracal/Super Cougar) Comparison

Aviation | Utilities | Side-by-Side Comparison

Direct side-by-side comparison of two aircraft.

Your selected aircraft are compared in side-by-side arrangement below. You can always go back and Compare any two aircraft in our database. Some entries contain '0', 'not available', or an 'NA' value. This is more common with conceptual, experimental, and x-plane designs. Rotary-wing system (i.e. helicopters) values include main rotor diameter as part of width/wingspan measurement. UAV entries may display crew values as '0', not taking into account ground-based controllers.

Subjects

Mil Mi-17 (Hip-H)
Medium-Lift Transport Helicopter / Gunship

Eurocopter EC725
Medium Transport Helicopter

Basics

ORIGIN
Soviet Union

ORIGIN
France

YEAR
1981 [Diff.-24 yrs]

YEAR
2005 [Diff.+24 yrs]

CREW
3

CREW
2

PRODUCTION
12,000 units [Diff.+11,870]

PRODUCTION
130 units [Diff.-11,870]

Dimensions

LENGTH
60.5 ft (18.5 m) [Diff.-3.4 ft]

LENGTH
64.0 ft (19.5 m) [Diff.+3.4 ft]

HEIGHT
15.6 ft (4.8 m) [Diff.+0.5 ft]

HEIGHT
15.1 ft (4.6 m) [Diff.-0.5 ft]

Relative Size Comparison

Shapes below depict aircraft from wingtip-to-wingtip / nose-to-tail assuming aircraft are being viewed from overhead perspective (the nose pointing towards the top of the screen). Helicopter widths include main rotor diameter. If any dimensional values are "NA" in the database then the presented shapes may appear skewed.

Mil Mi-17 (Hip-H)

Eurocopter EC725

Weights

EMPTY WT.
16,535 lb (7,500 kg) [Diff.+4,784 lb]

EMPTY WT.
11,751 lb (5,330 kg) [Diff.-4,784 lb]

M.T.O.W.
29,762 lb (13,500 kg) [Diff.+5,071 lb]

M.T.O.W.
24,692 lb (11,200 kg) [Diff.-5,071 lb]

Installed Power

2 x Klimov TV3-117MT/VM OR VK-2500 turboshaft engines developing 2,100 shp or 2,700 shp respectively while driving five-bladed main rotor and three-bladed tail rotor.

2 x Turbomeca Makila 2A1 turboshaft engines developing 2,400 horsepower to a five-bladed main rotor and four-bladed tail rotor.

Performance

SPEED
158 mph (255 kph) [Diff.-43 mph]

SPEED
201 mph (324 kph) [Diff.+43 mph]

RANGE
360 miles (580 km) [Diff.-174 miles]

RANGE
534 miles (860 km) [Diff.+174 miles]

CEILING
19,685 ft (6,000 m) [Diff.-328 feet]

CEILING
20,013 ft (6,100 m) [Diff.+328 feet]

RATE-OF-CLIMB
1,575 ft/min [Diff.+865 feet]

RATE-OF-CLIMB
710 ft/min [Diff.-865 feet]

Armament

Typically none unless outfitted for gunship/armed transport role: Missiles (Shturm-V), rockets (S-8), rocket pods, 23mm cannon pods, and 7.62mm gun pods across underwing hardpoints when fitted wingstubs; 7.62mm machine guns at doors and / or rear of aircraft. Optional nose machine gun and fuel tanks.

Typically none. Though optional armament includes any one of the following packages:

2 x 7.62mm Fabrique Nationale FN MAG General Purpose Machine Guns on pintle mountings at side windows.
2 x 68mm 19-shot rocket pods on external side mounts.
2 x 20mm GIAT automatic cannon pods on external side mounts.

Going Further

View Entry
(Mil Mi-17 (Hip-H))

View Entry
(Airbus Helicopters H725/EC725 (Caracal/Super Cougar))

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Airbus H225 (Super Puma)

Aerospatiale SA330 Puma

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