Mi-8

General characteristics

Crew: 3 (pilot, copilot, flight engineer)

Capacity: ** 26 passengers or 12 stretchers and seat for 1 medical attendant or 4,000 kg (8,800 lb) on internal/external hardpoints

Length: 18.17 m (59 ft 7 in)

Rotor diameter: 21.29 m (69 ft 10 in)

Height: 5.65 m (18 ft 6 in)

Disc area: 356 m² (3,832 ft²)

Empty weight: 7,260 kg (16,007 lb)

Loaded weight: 11,100 kg (24,470 lb)

Max. takeoff weight: 13,000 kg] (26,659 lb)

Powerplant: 2 × Klimov TV3-117Mt turboshafts, 1,454 kW (1,950 shp)

Fuel max total capacity: 3,700 l (977 US gal)

 

Performance

Maximum speed: 260 km/h (140 kt)

Cruise speed: 123 knots, 141 mph (230 km/h[54])

Range: 328 nm, 378 mi (610 km[55])

Ferry range: 960 km (596 mi)

Serviceceiling: 4,500 m (14,765 ft)

 

Armament

4,000 kg (9,900 lb) of disposable stores on six hardpoints, including 57 mm S-5 rockets, bombs, or 9M17 Phalanga ATGMs.

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Mi-17/17-1V, Мi-171/172

General characteristics

Crew: Three – two pilots and one engineer

Capacity: 24 troops or 12 stretchers or 4,000 kg (8,820 lb) cargo internally /5,000 kg (11,023 lb) externally slung.

Length: 18.465 m (60 ft 7 in)

Rotor diameter: 21.25 m (69 ft 10½ in)

Height: 4.76 m (15 ft 7¼ in)

Disc area: 356 m² (3,834 ft²)

Empty weight: 7,489 kg (16,510 lb)

Loaded weight: 11,100 kg (24,470 lb)

Max. takeoff weight: 13,000 kg (28,660 lb)

Powerplant: 2 × VK-2500PS-03 turboshaft, 2,400 hp each

 

Performance

Maximum speed: 280 km/h (151 knots, 174 mph)

Cruise speed: 260 km/h

Range: 800 km (431 nmi, 497 mi) (with main fuel tanks)

Service ceiling: 6,000 m (19,690 ft)

Rate of climb: 8 m/s[citation needed] (1,575 ft/min)

KA-32

Performance

Max. speed 260 km/h

Cruise speed (at maximum range) 200 km/h

Cruise speed (at maximum continuous engine power) 245 km/h

Maximum flight range with main fuel tanks 650 km

Maximum flight height 5,000 m

 

Weight Parameters

Max. take-off weight 11,000 kg

With underslung load 12,700 kg

Max. Payload, kg in transport cabin 3,700 on external sling 5,000

Engines 2хTV3-117 VMA

Take-off power 2,200 h. p.

Contingency power 2,400 h. p.

Dimensions of СargoСabin:

Length 4520 mm

Maximum floor width 1,300 mm

Height 1,240 mm

Volume 7.3 m3

 

Capacity:

Aircrew 1–2 persons

Service passengers up to 13 persons

MI-26

General characteristics

Crew: Five: 2 pilots, 1 navigator, 1 flight engineer, 1 flight technician

 

Capacity:

90 troops or 60 stretchers

20,000 kg cargo (44,090 lb)

Length: 40.025 m (131 ft 3¾ in) (rotors turning)

Rotor diameter: 32.00 m (105 ft 0 in)

Height: 8.145 m (26 ft 8¾ in)

Disc area: 804.25 m2 (8,656.8 ft²)

Empty weight: 28,200 kg (62,170 lb)

Loaded weight: 49,600 kg (109,350 lb)

Max. takeoff weight: 56,000 kg (123,450 lb)

Powerplant: 2 × Lotarev D-136 turboshafts, 8,500 kW (11,399 shp) each

Main rotor RPM: 132

 

Performance

Maximum speed: 295 km/h (159 kn, 183 mph)

Cruise speed: 255 km/h (137 kn, 158 mph)

Range: 1,920 km (1,036 nmi, 1,190 mi) (with auxiliary tanks)

Serviceceiling: 4,600 m (15,100 ft)

CONTACT US!

Phone: +7 495 660 08 58

Email: info@techno2000rus.ru

Fax: +7 495 660 08 58

 

Russia, Moscow region,

city district Khimki, md. Klyazma, d. 1B,

Industrial Park "Sheremetyevo"