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Original uploader was User:Ahunt at en:wikipedia · Public domain · Resized · Public domain · Source ↗ · Modified
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At a glance
Measured figures
F28F · Length
Single source29 ft 3 in (8.92 m)[source]
Ka-126 · Length
Single sourceConfiguration
| Specification | Enstrom F-28 | Kamov Ka-126 |
|---|---|---|
| Type | Light helicopter[source] | Light utility helicopter[source] |
| Manufacturer | Enstrom Helicopter Corporation[source] | Industria Aeronautică Română[source] |
| Manufactured | 1965-present[source] | 1988–1991[source] |
| Introduction date | 1965[source] | 1989 |
7.775 m (25 ft 6 in)[source]
F28F · 1 × Lycoming HIO-360-F1AD four-cylinder, direct-drive, horizontally opposed, air-cooled, piston aircraft engine
Single source1 × Lycoming HIO-360-F1AD four-cylinder, direct-drive, horizontally opposed, air-cooled, piston aircraft engine, 225 hp (168 kW)[source]
Ka-126 · 1 × Omsk TVO-100 turboshaft
Single source1 × Omsk TVO-100 turboshaft , 522 kW (700 hp)[source]
F28F · Endurance
Single source3 hr 30 min[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Variants | Enstrom TH180 Spitfire Mark I[source] | — |
|---|
| Developed into | Enstrom 480[source] | Kamov Ka-226[source] |
|---|
| Capacity | two 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] |
|---|
| Main rotor area | 804 sq ft (74.7 m 2 ) NACA 0013.5[source] | 265.5 m 2 (2,858 sq ft)[source] |
|---|
| Country of origin | Vereinigte Staaten[source]Country of design · Entwurfsland | — |
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| Designer | — | Kamov[source] |
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| Status | — | Active[source] |
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| Number built | — | 17[source] |
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| First flight | — | 22 December 1988[source] |
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| Developed from | — | Kamov Ka-26[source] |
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| Blade sections | — | NACA 23015 modified root, NACA 23012 modified tip[source] |
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| Role | — | Soviet light utility helicopter[source] |
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| National origin | — | Soviet Union[source] |
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| 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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