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bomberpilot · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
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At a glance
Measured figures
Mi-2T · Length
Single source11.4 m (37 ft 5 in)[source]
S-92 · Length
Single sourceConfiguration
| Specification | Mil Mi-2 | Sikorsky S-92 |
|---|---|---|
| Type | Utility helicopter[source] | Medium-lift transport/utility helicopter[source] |
| Designer | Mil Moscow Helicopter Plant[source] | — |
| Built by | PZL-Świdnik[source] | — |
| Status | In service[source] | In service[source] |
| Primary users | Soviet Air Force (historical) Polish Armed Forces Aeroflot (historical)[source] |
68 ft 6 in (20.88 m)[source]
S-92 · fuselage
Single source17 ft 3 in (5.26 m) fuselage[source]
Empty; Mi-2T · Empty weight
Single sourceGross; Mi-2T · Gross weight
Single sourceMaximum take-off; Mi-2T · Max takeoff weight
Single source2,372 kg (5,229 lb)[source]
3,550 kg (7,826 lb)[source]
3,700 kg (8,157 lb)[source]
Empty; S-92 · Empty weight
Single sourceGross; S-92 · Gross weight
Single sourceMi-2T · 2 × PZL GTD-350P turboshaft engines (400 shp) each
Single source2 × PZL GTD-350P turboshaft engines, 300 kW (400 shp) 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]
Mi-2T · 890 ft/min
Single source4.5 m/s (890 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
CHC Helicopter Petroleum Helicopters International Bristow Helicopters Cougar Helicopters[source] |
| Number built | 5,497[source] | at least 300[source] |
|---|
| Manufactured | 1964–1998[source] | 1998–present[source] |
|---|
| Introduction date | 1965[source] | 2004[source] |
|---|
| First flight | 22 September 1961[source] | December 23, 1998[source] |
|---|
| Developed from | Mil Mi-1[source] | Sikorsky S-70[source] |
|---|
| Variant | PZL Kania[source] | — |
|---|
| Capacity | 8 passengers / 700 kg (1,543 lb) internal cargo / 800 kg (1,764 lb) external cargo[source] | 19 passengers[source] |
|---|
| Main rotor area | 165.15 m 2 (1,777.7 sq ft)[source] | 2,492.3 sq ft (231.54 m 2 )[source] |
|---|
| Blade section | NACA 23012M[source] | - root: Sikorsky SC2110; tip: Sikorsky SSC-A09[source] |
|---|
| Disk loading | 22.41 kg/m 2 (4.59 lb/sq ft)[source] | 9.8 lb/sq ft (48 kg/m 2 )[source] |
|---|
| Power/mass | 0.0806 kW/kg (0.0490 hp/lb)[source] | 0.23 hp/lb (0.38 kW/kg)[source] |
|---|
| Country of origin | Soviet Union[source] | — |
|---|
| Manufacturer | PZL-Świdnik[source] | Sikorsky Aircraft[source] |
|---|
| National origin | — | United States[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] |
|---|
Maximum take-off; S-92 · Max takeoff weight
Single source