Credit
Alex Snow · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
Mi-38 · excluding rotors
Single source20.282 m (66 ft 7 in) excluding rotors[source]
S-92 · Length
Single sourceConfiguration
| Specification | Mil Mi-38 | Sikorsky S-92 |
|---|---|---|
| Type | Medium transport helicopter[source] | Medium-lift transport/utility helicopter[source] |
| National origin | Russia[source] | United States[source] |
| Manufacturer | Kazan Helicopters[source] | Sikorsky Aircraft[source] |
| Designer | Mil Moscow Helicopter Plant[source] | — |
| Status |
68 ft 6 in (20.88 m)[source]
S-92 · fuselage
Single source17 ft 3 in (5.26 m) fuselage[source]
Mi-38 · 2 × Klimov TV7-117 V turboshaft engines each
Single source2 × Klimov TV7-117 V turboshaft engines, 2,100 kW (2,800 hp) each[source]
S-92 · 2 × General Electric CT7-8A turboshaft engines, 2,520 shp ( ) each
Single source2 × General Electric CT7-8A turboshaft engines, 2,520 shp (1,880 kW) each[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
In service[source] |
In service[source] |
| Primary users | Russian Air Force Myanmar Air Force[source] | CHC Helicopter Petroleum Helicopters International Bristow Helicopters Cougar Helicopters[source] |
|---|
| Number built | 16 (4 prototypes, 12 serial production units)[source] | at least 300[source] |
|---|
| Manufactured | 2003–present[source] | 1998–present[source] |
|---|
| Introduction date | 2 December 2019 (Mi-38T)[source] | 2004[source] |
|---|
| First flight | 22 December 2003[source] | December 23, 1998[source] |
|---|
| Variant | Mi-38T[source] | — |
|---|
| Capacity | 30 max / 6,000 kg (13,000 lb) internal payload / 7,000 kg (15,000 lb) external payload[source] | 19 passengers[source] |
|---|
| Main rotor area | 349.67 m 2 (3,763.8 sq ft)[source] | 2,492.3 sq ft (231.54 m 2 )[source] |
|---|
| Hover ceiling OGE | 3,100 m (10,200 ft)[source] | — |
|---|
| Disk loading | 44.6 kg/m 2 (9.1 lb/sq ft) max[source] | 9.8 lb/sq ft (48 kg/m 2 )[source] |
|---|
| Power/mass | 0.1675 kW/kg (0.1019 hp/lb)[source] | 0.23 hp/lb (0.38 kW/kg)[source] |
|---|
| Developed from | — | Sikorsky S-70[source] |
|---|
| Variants | — | Sikorsky CH-148 Cyclone Sikorsky VH-92[source] |
|---|
| Cabin dimensions | — | 20 ft (6 m) long by 6.6 ft (2 m) tall[source] |
|---|
| Blade section | — | - root: Sikorsky SC2110; tip: Sikorsky SSC-A09[source] |
|---|
Maximum take-off; S-92 · Max takeoff weight
Single source