Technical Data of Russian Helicopters

Light helicopters with MTOW up to 2500 kg  

Variant

Ka-8

Ka-10M

Ka-15

Ka-18

Mi-1M

Mi-34

Crew

1

1

1

1

1

1

Passengers

-

1

1

3

2 až 3

3

Fuselage lenght

3,7 m

3,7 m

6,26 m

7,03 m

12,10 m

8,71 m

Length with rotors turning

5,6 m

6,12 m

9,96 m

10,0 m

13,258 m

11,42 m

Height with rotors turning

2,5 m

2,5 m

3,35 m

3,4 m

3,3 m

2,75 m

Main rotor diameter

3,7 m

6,12 m

9,96 m

10,0 m

14,346 m

10,0 m

Tail rotor diameter

-

-

-

-

2,50 m

1,48 m

Empty weight

183 kg

249 kg

968 kg

1040 kg

1798 kg

800 kg

Maximum take off weight

275 kg

390 kg

1370 kg

1502 kg

2296 kg

1350 kg

Engines – type

M-75

AI-4V

AI-14V

AI-14VF

AI-26V

M-14V-26

Engines – number

1

1

1

1

1

1

Engines – output

20 kW

40 kW

168 kW

206 kW

422 kW

239 kW

Maximum speed

80 km/h

115 km/h

155 km/h

160 km/h

190 km/h

210 km/h

Cruise speed

-

90 km/h

120 km/h

130 km/h

140 km/h

180 km/h

Ceiling – hovering

250 m

2500 m

600 m

600 m

2000 m

1500 m

Ceiling – dynamic

50 m

100 m

3500 m

3500 m

4000 m

4500 m

Range

40 km

170 km

350 km

450 km

350 km

450 km

Medium helicopters with MTOW up to 8000 kg   

Variant

Ka-26

Ka-226

Ka-25PL

Ka-60

Mi-2T

Mi-4A

Crew

1

1

2+2

2

1

2+1

Passengers

6

7

-

16

7 až 8

12

Fuselage lenght

7,75 m

8,1 m

9,75 m

13,47 m

11,94 m

16,80 m

Length with rotors turning

13,0 m

13,0 m

15,74 m

15,64 m

17, 42 m

25,02 m

Height with rotors turning

4,05 m

4,15

5,37

4,0 m

4,53 m

5,18 m

Main rotor diameter

13,0 m

13,0 m

15,74 m

13,5 m

14,56 m

21 m

Tail rotor diameter

-

-

-

1,4 m

2,70 m

3,6 m

Empty weight

1950 kg

-

4765 kg

3500 kg

2372 kg

5250 kg

Maximum take off weight

3250 kg

3400 kg

7500 kg

6500 kg

3550 kg

7600 kg

Engines – type

M-14V-26

250-C20

GTD-3BM

RD-600

GTD-350

AŠ-82V

Engines – number

2

2

2

2

2

1

Engines – output

239 kW

331 kW

738 kW

975 kW

295 kW

1250 kW

Maximum speed

170 km/h

205 km/h

220 km/h

300 km/h

210 km/h

185 km/h

Cruise speed

130 km/h

195 km/h

195 km/h

245 km/h

180 km/h

160 km/h

Ceiling – hovering

640 m

2500 m

600 m

2100 m

1600 m

2000 m

Ceiling – dynamic

2700 m

6500 m

4000 m

5150 m

4000 m

5500 m

Range

520 km

600 km

650 km

700 km

370 km

406 km

Heavy helicopters with MTOW over 8000 kg  

Variant

Ka-27PL

Jak-24

Mi-8T

Mi-17

Mi-14PL

Mi-38

Crew

2+1

2+1

3

3

4

2

Passengers

-

40

24

38-36

20

30

Fuselage lenght

12,25 m

21,34 m

18,31 m

18,31 m

18,37 m

19,95 m

Length with rotors turning

15,90 m

33,03 m

25,31 m

25,31 m

25,315 m

25,22 m

Height with rotors turning

5,4 m

6,5 m

5,60 m

5,60 m

6,94 m

5,13 m

Main rotor diameter

15,90 m

20 m

21,29 m

21,29 m

21,29 m

21,1 m

Tail rotor diameter

-

-

3,9 m

3,9 m

3,9 m

3,84 m

Empty weight

6100 kg

10607 kg

7260 kg

7200 kg

8902 kg

8300 kg

Maximum take off weight

12000 kg

14270 kg

12000 kg

13000 kg

14000 kg

15600 kg

Engines – type

TV3-117KM

AŠ-82V

TV2-117A

TV3-117MT

TV3-117M

TVA-3000

Engines – number

2

2

2

2

2

2

Engines – output

1636 kW

1250 kW

1103 kW

1397 kW

1397 kW

1838 kW

Maximum speed

291 km/h

175 km/h

250 km/h

250 km/h

230 km/h

290 km/h

Cruise speed

250 km/h

156 km/h

225 km/h

220 km/h

210 km/h

275 km/h

Ceiling – hovering

3500 m

2000 m

1000 m

1760 m

1200 m

2500 m

Ceiling – dynamic

5000 m

4200 m

4500 m

5000 m

4000 m

5200 m

Range

760 km

265 km

520 km

580 km

400 km

800 km

Super heavy helicopters

Variant

Ka-22

Mi-6A

Mi-10

Mi-10K

V-12

Mi-26T

Crew

5

5

5

5

6

4

Passengers

80

90

28

28

196

82

Fuselage lenght

33,16 m

32,86 m

32,4 m

37,0 m

33,75 m

Length with rotors turning

26,75 m

41,74 m

41 m

39 m

-

40,03 m

Height with rotors turning

10,38 m

9,16 m

7,8 m

7,8 m

12,5 m

8,1 m

Main rotor diameter

22,5 m

35 m

35 m

35 m

35  m

32 m

Tail rotor diameter

23,8 m

6,3 m

6,3 m

6,3 m

-

7,61 m

Empty weight

24430 kg

27500 kg

27100 kg

25450 kg

69100 kg

28150 kg

Maximum take off weight

42500 kg

44000 kg

43550 kg

38000 kg

105000 kg

56000 kg

Engines – type

D-25VK

D-25V

D-25V

D-25V

D-25VF

D-136

Engines – number

2

2

2

2

4

2

Engines – output

4050 kW

4101 kW

4101 kW

4101 kW

4847 kW

11400 kW

Maximum speed

365 km/h

300 km/h

335 km/h

350 km/h

260 km/h

295 km/h

Cruise speed

256 km/h

250 km/h

180 km/h

228 km/h

240 km/h

255 km/h

Ceiling – hovering

1270 m

1000 m

3000 m

2200 m

600 m

2900 m

Ceiling – dynamic

5500 m

4500 m

4750 m

3000 m

3500 m

4600 m

Range

450 km

620 km

430 km

500 km

1000 km

1800 km

Attack helicopters

Variant

Ka-29TB

Ka-50

Mi-24V

Mi-28N

Mi-8AMTŠ

Crew

2

1

2 až 3

2

3

Passengers

16

-

8

-

36

Fuselage lenght

11,6

14,21 m

17,31 m

16,85 m

18,31 m

Length with rotors turning

15,90 m

15,96 m

21,35 m

21,16 m

25,31 m

Height with rotors turning

5,4 m

4,9 m

5,47 m

4,81 m

5,60 m

Main rotor diameter

15,90 m

14,45 m

17,3 m

17,2 m

21,29 m

Tail rotor diameter

-

-

3,9 m

4,81 m

3,9 m

Empty weight

5520 kg

7700 kg

8620 kg

8590 kg

7260 kg

Maximum take off weight

11500 kg

10800 kg

11800 kg

12000 kg

12200 kg

Engines – type

280 km/h

310 km/h

335 km/h

324 km/h

250 km/h

Engines – number

230 km/h

270 km/h

295 km/h

265 km/h

220 km/h

Engines – output

TV3-117VK

TV3-117VMA

TV3-117V

VK-2500

TV3-117MT

Maximum speed

2

2

2

2

2

Cruise speed

1660 kW

1789 kW

1640 kW

1766 kW

1397 kW

Ceiling – hovering

3700 m

4000 m

1500 m

3700 m

1900 m

Ceiling – dynamic

5000 m

5500 m

4800 m

5700 m

4500 m

Range

800 km

455 km

450 km

435 km

580 km

Range with aux. fuel tanks

-

1100 km

1000 km

1105 km

-