Credit
Ronnie Robertson · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
EC175 · rotors running
Single source18.06 m (59 ft 3 in) rotors running[source]
Ka-126 · Length
Configuration
| Specification | Airbus Helicopters H175 | Kamov Ka-126 |
|---|---|---|
| Type | Medium utility helicopter[source] | Light utility helicopter[source] |
| National origin | Multinational[source] | Soviet Union[source] |
| Manufacturer | Eurocopter Airbus Helicopters Aviation Industry Corporation of China[source] | Industria Aeronautică Română[source] |
| Status | In service[source] |
7.775 m (25 ft 6 in)[source]
Empty; EC175 · Empty weight
Single sourceGross; EC175 · Gross weight
Single sourceMaximum take-off; EC175 · Max takeoff weight
Single source4,603 kg (10,148 lb)[source]
7,500 kg (16,535 lb)[source]
7,800 kg (17,196 lb)[source]
Empty; Ka-126 · Empty weight
Single sourceMaximum take-off; Ka-126 · Max takeoff weight
Single sourceEC175 · 2 × Pratt & Whitney Canada PT6C-67E turboshaft engines with dual channel FADEC each for take-off
Single source2 × Pratt & Whitney Canada PT6C-67E turboshaft engines with dual channel FADEC, 1,324 kW (1,776 hp) each for take-off[source]
Ka-126 · 1 × Omsk TVO-100 turboshaft
Single source1 × Omsk TVO-100 turboshaft , 522 kW (700 hp)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Active[source]
| Manufactured | 2009–present[source] | 1988–1991[source] |
|---|
| Introduction date | H175 : December 2014[source] | 1989[source] |
|---|
| First flight | H175: 17 December 2009 AC352: 20 December 2016[source] | 22 December 1988[source] |
|---|
| Capacity | 12-18 pax[source] up to 18 passengers[source] | 6 passengers (cargo/passenger pod) / 1,000 kg (2,205 lb) slung load / 1,000 L (260 US gal; 220 imp gal) chemical hopper[source] |
|---|
| Fuel capacity | 2,710 L (720 US gal; 600 imp gal) / 2,136 kg (4,709 lb)[source] | — |
|---|
| Main rotor area | 172 m 2 (1,850 sq ft)[source] | 265.5 m 2 (2,858 sq ft)[source] |
|---|
| Designer | — | Kamov[source] |
|---|
| Number built | — | 17[source] |
|---|
| Developed from | — | Kamov Ka-26[source] |
|---|
| Developed into | — | Kamov Ka-226[source] |
|---|
| Blade sections | — | NACA 23015 modified root, NACA 23012 modified tip[source] |
|---|
| Role | — | Soviet light utility helicopter[source] |
|---|
| Source measurement | — | One or two crew utility light helicopter, powered by a 720-shp (537-kW) (Glushenkov) OMKB TVD-100 turboshaft engines. First flown in 1986, and built under licence by IAR in Romania . 2 prototypes and 15 series helicopter built.[source]Kamov Ka-126 · Variants; only the objects and conditions stated in this passage One prototype, powered by a 722-shp (538-kW) Turbomeca Arriel 1D1 turboshaft engine.[source]Kamov Ka-126 · Variants; only the objects and conditions stated in this passage Powered by two 450-shp (335-kW) Rolls-Royce 250-C20R/2 turboshaft engines.[source]Kamov Ka-126 · Variants; only the objects and conditions stated in this passage The V-60 was a projected light (3500 kg) armed escort helicopter from Kamov based on the civil Kamov Ka-126. Only a model of the original V-60 exists. The existing model shows four missiles as its sole armament. The project was abandoned in the 1980s and is often confused to be an early concept of the Ka-60 . The initial prototype and pre-series version of the Ka-60 carried another designation, V-62 .[source]Kamov Ka-126 · Variants / Kamov V-60; only the objects and conditions stated in this passage Capacity: 6 passengers (cargo/passenger pod) / 1,000 kg (2,205 lb) slung load / 1,000 L (260 US gal; 220 imp gal) chemical hopper[source]Kamov Ka-126 · Specifications (Ka-126); only the objects and conditions stated in this passage Length: 7.775 m (25 ft 6 in)[source]Kamov Ka-126 · Specifications (Ka-126); only the objects and conditions stated in this passage Height: 4.155 m (13 ft 8 in)[source]Kamov Ka-126 · Specifications (Ka-126); only the objects and conditions stated in this passage Empty weight: 1,915 kg (4,222 lb)[source]Kamov Ka-126 · Specifications (Ka-126); only the objects and conditions stated in this passage Max takeoff weight: 3,250 kg (7,165 lb)[source]Kamov Ka-126 · Specifications (Ka-126); only the objects and conditions stated in this passage Powerplant: 1 × Omsk TVO-100 turboshaft , 522 kW (700 hp)[source]Kamov Ka-126 · Specifications (Ka-126); only the objects and conditions stated in this passage Main rotor diameter: 2 × 13 m (42 ft 8 in)[source]Kamov Ka-126 · Specifications (Ka-126); only the objects and conditions stated in this passage Main rotor area: 265.5 m 2 (2,858 sq ft)[source]Kamov Ka-126 · Specifications (Ka-126); only the objects and conditions stated in this passage Maximum speed: 180 km/h (110 mph, 97 kn)[source]Kamov Ka-126 · Specifications (Ka-126); only the objects and conditions stated in this passage Cruise speed: 160 km/h (99 mph, 86 kn)[source]Kamov Ka-126 · Specifications (Ka-126); only the objects and conditions stated in this passage Range: 713 km (443 mi, 385 nmi)[source]Kamov Ka-126 · Specifications (Ka-126); only the objects and conditions stated in this passage Service ceiling: 3,850 m (12,630 ft)[source]Kamov Ka-126 · Specifications (Ka-126); only the objects and conditions stated in this passage Rate of climb: 6.6 m/s (1,300 ft/min)[source]Kamov Ka-126 · Specifications (Ka-126); only the objects and conditions stated in this passage |
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| Reported operators |
| — |
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