Mil Mi-10 vs Sikorsky CH-148 Cyclone: Specs Compared

Mil Mi-10 — licensed reference photograph

AHelicopters

Mil Mi-10

Aerial crane

Credit

Unknown author Unknown author · Public domain · Resized · Public domain · Source ↗ · Modified

Sikorsky CH-148 Cyclone — licensed reference photograph

BHelicopters

Sikorsky CH-148 Cyclone

Maritime helicopter

Credit

Mass Communication Specialist Seaman Santiago Navarro · Public domain · Resized · Public domain · Source ↗ · Modified

First system

Second system

At a glance

Side by side

Length comparisonOne shared metre scale

Mil Mi-10Mi-10 · overall length, rotors turning

41.89 m

Length source ↗

Sikorsky CH-148 CycloneCH-148 Cyclone · Length

17.22 m

Length source ↗

Lengths retain their source configuration and measurement scope.

Measured figures

Head to head

19 of 26 rows sourced on both sides

41.89mMi-10 · overall length, rotors turning

17.22mCH-148 Cyclone · Length

LengthScopes differ

All recorded figures & sources

32.86 m

Mi-10 · fuselage only

Single source

41.89 m

Mi-10 · overall length, rotors turning

Single source

32.86 m (107 ft 10 in) (fuselage only), 41.89 m (137 ft 5 in) (overall length, rotors turning)^[source]

17.22 m

CH-148 Cyclone · Length

Single source

17.12 m

Length

Single source

56 ft 2 in (17.12 m) .^[source]

17.22 m^[source]CH-148 Cyclone

—

5.26mfuselage

Width

All recorded figures & sources

5.26 m

fuselage

Single source

17 ft 3 in (5.26 m) fuselage^[source]

35mMi-10 · Main rotor diameter

17.7mMain rotor diameter

Rotor diameterScopes differ

All recorded figures & sources

35 m

Mi-10 · Main rotor diameter

Single source

35.00 m (114 ft 10 in)^[source]

17.48 m

CH-148 Cyclone · Rotor diameter · Rotor span

Single source

17.7 m

Main rotor diameter

Single source

58 ft 1 in (17.70 m)^[source]

17.48 m^[source]CH-148 Cyclone · Rotor span

9,9 м (с остановленным хвостовым винтом)

5.44mCH-148 Cyclone · Height

Height

All recorded figures & sources

9,9 м (с остановленным хвостовым винтом)^[source]

5.44 m

CH-148 Cyclone · Height

Single source

4.7 m

S-92

Single source

15 ft 5 in (4.70 m) S-92^[source]

5.44 m^[source]CH-148 Cyclone

43.7t

13.3tMaximum take-off; Max takeoff weight

MassScopes differ

All recorded figures & sources

27,100 kg

Empty; Mi-10 · Empty weight

Single source

25,450 kg

Empty; Mi-10 · Mi-10K

Single source

43,550 kg

Gross; Mi-10 · Gross weight

Single source

37,000 kg

Gross; Mi-10 · Mi-10K

Single source

43,700 kg

Maximum take-off; Mi-10 · Max takeoff weight

Single source

38,000 kg

Maximum take-off; Mi-10 · Mi-10K

Single source

27,100 kg (59,745 lb) , Mi-10K 25,450 kg (56,110 lb)^[source]

43,550 kg (96,011 lb) , Mi-10K 37,000 kg (82,000 lb)^[source]

43,700 kg (96,342 lb) , Mi-10K 38,000 kg (84,000 lb)^[source]

7,076 kg

Empty; S-92

Single source

13,000 kg

Gross; CH-148 Cyclone · Gross weight · Maximum gross weight

Single source

13,290 kg

Maximum take-off; Max takeoff weight

Single source

15,600 lb (7,076 kg) S-92^[source]

29,300 lb (13,290 kg)^[source]

13,000 kg^[source]CH-148 Cyclone · Maximum gross weight

CrewScopes differ

All recorded figures & sources

3 people

Mi-10 · pilot, copilot and flight engineer, navigator/radio operator and optional technician

Single source

3 (pilot, copilot and flight engineer, navigator/radio operator and optional technician)^[source]

4 people

2 pilots; 1 tactical coordinator, ACSO; 1 sensor operator, AES OP

Single source

4 (2 pilots; 1 tactical coordinator, ACSO; 1 sensor operator, AES OP)^[source]

335km/hMaximum; Mi-10 · Maximum speed

306km/hMaximum; Maximum speed

SpeedScopes differ

All recorded figures & sources

180 km/h

Cruise; Mi-10 · Cruise speed

Single source

335 km/h

Maximum; Mi-10 · Maximum speed

Single source

335 km/h (208 mph, 181 kn)^[source]

180 km/h (110 mph, 97 kn)^[source]

254 km/h

Cruise; Cruise speed

Single source

287 km/h

Maximum; CH-148 Cyclone · Maximum speed

Single source

306 km/h

Maximum; Maximum speed

Single source

165 kn (190 mph, 306 km/h)^[source]

137 kn (158 mph, 254 km/h)^[source]

287 km/h^[source]CH-148 Cyclone

430kmMi-10 · Range

740kmCH-148 Cyclone · Range

RangeScopes differ

All recorded figures & sources

430 km

Mi-10 · Range

Single source

430 km (270 mi, 230 nmi)^[source]

740 km

CH-148 Cyclone · Range

Single source

740 km^[source]CH-148 Cyclone

4,100kW

2,200kW

PowerScopes differ

All recorded figures & sources

4,100 kW

Mi-10 · 2 × Soloviev D-25V turboshaft each

Single source

2 × Soloviev D-25V turboshaft, 4,100 kW (5,500 hp) each^[source]

2,200 kW

2 × General Electric CT7-8A7 turboshaft engines, 3,000 shp ( ) each

Single source

2 × General Electric CT7-8A7 turboshaft engines, 3,000 shp (2,200 kW) each^[source]

3000 м

4,600m

Service ceiling

All recorded figures & sources

3000 м^[source]

4,600 m

Service ceiling

Single source

15,000 ft (4,600 m)^[source]

Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.

Configuration

Details

Mil Mi-10 and Sikorsky CH-148 Cyclone configuration
Specification	Mil Mi-10	Sikorsky CH-148 Cyclone
Type	Aerial crane^[source]	Maritime helicopter^[source]
National origin	Russia^[source]	United States^[source]
Manufacturer	Mil Moscow Helicopter Plant^[source]	Sikorsky Aircraft^[source]
Status	Active as of 2014 (Mi-10K)^[source]	In service^[source]
Number built	55^[source]	28^[source]
Manufactured	1964–69^[source]	—
Introduction date	1963^[source]	July 2018^[source]
First flight	15 June 1960^[source]	15 November 2008^[source]
Developed from	Mil Mi-6^[source]	Sikorsky S-92^[source]
Capacity	28 passengers or 3 t (3,000 kg; 6,600 lb) internally up to 15 t (15,000 kg; 33,000 lb) payload on platform or 8 t (8,000 kg; 18,000 lb) max slung payload^[source]	6 in mission configuration, up to 22 in utility configuration.^[source] 22 passengers^[source]
Ground clearance under fuselage	3.75 m (12 ft 4 in)^[source]	—
Main rotor area	962 m 2 (10,350 sq ft)^[source]	2,650 sq ft (246 m 2 ) S-92^[source]
Hovering ceiling out of ground effect	3,000 m (9,840 ft)^[source]	—
Primary user	—	Royal Canadian Air Force^[source]
Folded Length	—	14.78 m (48.5 ft)^[source]
Blade section	—	- root: Sikorsky SC2110; tip: Sikorsky SSC-A09 - S-92^[source]

FORCETALLY

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Mil Mi-10

Sikorsky CH-148 Cyclone

Type

Aerial crane^[source]

Maritime helicopter^[source]

National origin

Russia^[source]

United States^[source]

Manufacturer

Mil Moscow Helicopter Plant^[source]

Sikorsky Aircraft^[source]

Status

Active as of 2014 (Mi-10K)^[source]

In service^[source]

Number built

55^[source]

28^[source]

Manufactured

1964–69^[source]

—

Introduction date

1963^[source]

July 2018^[source]

First flight

15 June 1960^[source]

15 November 2008^[source]

Developed from

Mil Mi-6^[source]

Sikorsky S-92^[source]

Capacity

28 passengers or 3 t (3,000 kg; 6,600 lb) internally up to 15 t (15,000 kg; 33,000 lb) payload on platform or 8 t (8,000 kg; 18,000 lb) max slung payload^[source]

6 in mission configuration, up to 22 in utility configuration.^[source]

22 passengers^[source]

Ground clearance under fuselage

3.75 m (12 ft 4 in)^[source]

—

Main rotor area

962 m 2 (10,350 sq ft)^[source]

2,650 sq ft (246 m 2 ) S-92^[source]

Hovering ceiling out of ground effect

3,000 m (9,840 ft)^[source]

—

Primary user

—

Royal Canadian Air Force^[source]

Folded Length

—

14.78 m (48.5 ft)^[source]

Blade section

—

- root: Sikorsky SC2110; tip: Sikorsky SSC-A09 - S-92^[source]