| Specifications |
|---|
| Country of Origin |
Russia
|
| Builder |
Mil
|
| Crew | Six
|
| Length | 37.00 m (121 ft 4 in)
|
| Rotor diameter | 2 x 35.00 m (114 ft 10 in)
|
| Height | 12.50 m (41 ft 0 in)
|
| Disc area | 1,924 m² (20,700 ft²)
|
| Wingspan overall | 67 m
|
| internal main section | length 28.15 m, Width and height: 4,40 m 4.40 m
|
| Capacity | Up to 40,000 kg of cargo
|
| Payload, off Adava | 25 000 kg
|
| Off ADAC | 30 000 kg
|
| maximum load on sling | 5 500 kg
|
| Empty weight | 69,100 kg (152,020 lb)
|
| Loaded weight | 97,000 kg (213,400 lb)
|
| Max takeoff weight | 105,000 kg (231,000 lb)
|
| Powerplant | 4× Soloviev D-25VF turboshafts, 4,048 kW (6,497 shp) each
|
| Performance |
|
| Maximum speed | 260 km/h (163 mph)
|
| Maximum cruise speed | 240 km/h
|
| Range | 1,000 km (625 miles)
|
| Autonomy with 35,400 kg load | 500 km
|
| Service ceiling | 3,500 m (11,480 ft)
|
| Disc loading | 50 kg/m² (10 lb/ft²)
|
| Power/mass | 0.20 kW/kg (0.12 hp/lb)
|
