FORCETALLY
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At a glance
Measured figures
H160 · Length
Single source13.96 m (45 ft 10 in)[source]
CH-148 Cyclone · Length
Single sourceConfiguration
| Specification | Airbus Helicopters H160 | Sikorsky CH-148 Cyclone |
|---|---|---|
| Type | Medium utility helicopter[source] | Maritime helicopter[source] |
| National origin | Multinational[source] | United States[source] |
| Manufacturer | Airbus Helicopters[source] | Sikorsky Aircraft[source] |
| Status | In production[source] | In service |
Length
Single sourceCruise; H160 · Cruise speed
Single source255 km/h (158 mph, 138 kn)[source]
H160 · 2 × Safran Arrano 1A turboshaft engines (1,280 shp) each
Single source2 × Safran Arrano 1A turboshaft engines, 955 kW (1,280 shp) each[source]
2 × General Electric CT7-8A7 turboshaft engines, 3,000 shp ( ) each
Single source2 × General Electric CT7-8A7 turboshaft engines, 3,000 shp (2,200 kW) each[source]
H160 · with standard fuel tanks
Single source4 h 30 min with standard fuel tanks[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufactured | 2015–present[source] | — |
|---|
| Introduction date | 2021[source] | July 2018[source] |
|---|
| First flight | 13 June 2015[source] | 15 November 2008[source] |
|---|
| Capacity | 12[source] | 6 in mission configuration, up to 22 in utility configuration.[source] 22 passengers[source] |
|---|
| Useful load | up to 2,000 kg (4,400 lb)[source] | — |
|---|
| Fuel capacity | 1,120 kg (2,470 lb)[source] | — |
|---|
| Main rotor area | 141 m 2 (1,520 sq ft)[source] | 2,650 sq ft (246 m 2 ) S-92[source] |
|---|
| Never exceed speed | 315 km/h (196 mph, 170 kn)[source] | — |
|---|
| Disk loading | 42.9 kg/m 2 (8.8 lb/sq ft)[source] | — |
|---|
| Primary user | — | Royal Canadian Air Force[source] |
|---|
| Number built | — | 28[source] |
|---|
| Developed from | — | Sikorsky S-92[source] |
|---|
| Folded Length | — | 14.78 m (48.5 ft)[source] |
|---|
| Blade section | — | - root: Sikorsky SC2110; tip: Sikorsky SSC-A09 - S-92[source] |
|---|
Maximum take-off; Max takeoff weight
Single source