Credit
Col André Kritzinger · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Kazan Ansatlarger figure on 1 of 5
Sikorsky CH-148 Cyclonelarger figure on 4 of 5
Measured figures
Length
Single source13.76 m (45 ft 2 in)[source]
Length
Single sourceConfiguration
| Specification | Kazan Ansat | Sikorsky CH-148 Cyclone |
|---|---|---|
| Type | Multipurpose utility helicopter[source] | Maritime helicopter[source] |
| Manufacturer | Kazan Helicopters[source] | Sikorsky Aircraft[source] |
| Status | In service[source] | In service[source] |
| Primary user | Russian Aerospace Forces[source] | Royal Canadian Air Force |
Counts only measures both sources give with the same scope. A larger figure is not a better system.
CH-148 Cyclone · Length
Single sourcefuselage
Single source17 ft 3 in (5.26 m) fuselage[source]
2 × Pratt & Whitney Canada PW207K turboshaft engines (630 shp) each
Single source2 × Pratt & Whitney Canada PW207K turboshaft engines, 470 kW (630 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]
Endurance
Single source3 hours 07 minutes[source]
2,800 ft/min
Single source14 m/s (2,800 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufactured | 1998–present[source] | — |
|---|
| Introduction date | 28 August 2013[source] | July 2018[source] |
|---|
| First flight | 17 August 1999[source] | 15 November 2008[source] |
|---|
| Capacity | **7–8 passengers 2 stretchers and 3 attendants 1,235 kg (2,723 lb) internal[source] | 6 in mission configuration, up to 22 in utility configuration.[source] 22 passengers[source] |
|---|
| Fuel capacity | 535 kg[source] | — |
|---|
| Main rotor area | 103.87 m 2 (1,118.0 sq ft)[source] | 2,650 sq ft (246 m 2 ) S-92[source] |
|---|
| Never exceed speed | 275 km/h (171 mph, 148 kn)[source] | — |
|---|
| Hover ceiling OGE | 4,396 ft (1,340 m)[source] | — |
|---|
| National origin | Russia[source] | United States[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] |
|---|
Gross; CH-148 Cyclone · Gross weight · Maximum gross weight
Single source15,600 lb (7,076 kg) S-92[source]
29,300 lb (13,290 kg)[source]
13,000 kg[source]CH-148 Cyclone · Maximum gross weight
Maximum; CH-148 Cyclone · Maximum speed
Single source