The Kamov Ka-60 Kasatka (Russian: "Касатка", "Killer Whale"[3]) is a Russian medium twin-turbine military transport helicopter under development by Kamov. It performed its first flight on 24 December 1998.
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| Ka-60 Kasatka | |
|---|---|
 Kamov Ka-60 prototype at MAKS 2003 | |
| General information | |
| Type | Transport/utility helicopter |
| National origin | Russia |
| Manufacturer | Kamov |
| Number built | 2[1] |
| History | |
| First flight | 24 December 1998[2] |
The civil version is known as Kamov Ka-62.
Design
The Ka-60 has an estimated local military market of 200 units (Army aviation units, Border Police and the Ministry of Internal Affairs).[citation needed] The Ka-60 is to be used for aerial reconnaissance, for transporting air-assault forces, radio-electronic jamming, for special-operations missions and for various light-transport missions. Variations for foreign sale are expected. Manufacture is to take place at Ulan-Ude.
The civil version, the 6.8 t (15,000 lb) Ka-62, can carry up to 15 passengers or 2–2.5 t (4,400–5,500 lb) of cargo (internally or externally), has a top speed of 167 kn (310 km/h) and a range of 380 nmi (700 km).[4] It features a five-blade main rotor and shrouded tail rotor, and is powered by a pair of Safran Ardiden 3Gs, and later by in-development Klimov VK-1600s.[4] It has a 30-minute run-dry gearbox by Zoerkler, and can operate on one engine up to 9,500 ft (2,900m).[5]
Development
The development of the helicopter was long. The program started in 1984, but the first prototype Ka-60-01 flew in December 1998, and the second in 2007.[6]
A civil version, the Ka-62, was initially proposed when the Ka-60 programme was launched, but no production followed owing to development problems with the Ka-60's Saturn RD-600V 1500 hp engines. Instead, an agreement was signed in April 2011 to use the 1,306 kW (1,751 hp) Turbomeca Ardiden 3G turboshaft for a revised Ka-62. The main rotor will be driven via a new transmission, while the helicopter will have a revised cabin with larger windows and new avionics. First flight of the Ka-62 was planned for May 2013, with certification in 2014. Four prototypes and an initial batch of 16 Ka-62s for the Russian Ministry of Defence were planned,[7] with another 12 ordered by South American civilian customers. Russian certification was expected in 2018, with European EASA certification following in 2020.[8]
The Ka-62 was unveiled in 2012 and flight tests began in 2017.[4] After 434 test flights with three prototypes during 700h, it was certified on 30 November 2021 by Russian regulator Rosaviatsia.[4] Deliveries should begin in 2022, planned production is six units in 2022, eight in 2023 and 10 in 2024.[4] A cargo hook, a winch, a medical module and an anti-icing system should be certified until 2024.[4]
The development and certification of the Ka-62 was stopped in late 2022 due to Western sanctions and the large number of foreign-made components (including the French-manufactured engine).[9]
Variants
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- Ka-60
- Basic multi-role model.
- Ka-60U
- Training version.
- Ka-60K
- Naval version.
- Ka-60R
- Reconnaissance version.
- Ka-62
- New version for the civilian market. It has a redesigned fuselage with a high degree of composites, a larger cabin than the earlier demonstrators and will be equipped with Turbomeca Ardiden 3G engines.[10]
- Ka-64 Sky Horse
- Western certified export version equipped with two General Electric T700/CT7 turboshaft engines and five-blade main rotor.
Operators
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- Russian Aerospace Forces (100 on order)[11][12]
- Atlas Taxi Aereo (7 on order)[13]
- Vertical de Aviación (5 on order)[14]
Specifications
Data from Jane's All The World's Aircraft 2003–2004,[2] Russian Helicopters[10]
General characteristics
- Crew: 1 or 2
- Capacity: 12–15 passengers (Ka-62)
- 14 infantry troops or 6 stretchers
- Internal 2,000 kg (4,409 lb)
- External 2,500 kg (5,512 lb)
- Length: 15.6 m (51 ft 2 in) overall
- Height: 4.6 m (15 ft 1 in)
- Max takeoff weight: 6,500 kg (14,330 lb)
- Powerplant: 2 × Turbomeca Ardiden 3G turboshaft, 1,324 kW (1,776 shp) each
- Main rotor diameter: 13.5 m (44 ft 3 in)
- Main rotor area: 143.1 m2 (1,540 sq ft)
Performance
- Maximum speed: 308 km/h (191 mph, 166 kn)
- Cruise speed: 290 km/h (180 mph, 160 kn)
- Range: 770 km (480 mi, 420 nmi)
- Service ceiling: 5,700 m (18,700 ft)
- Hover ceiling: 3,300 m (10,827 ft)
See also
Aircraft of comparable role, configuration, and era
- AgustaWestland AW139
- Airbus Helicopters H155
- Bell 430
- Bell UH-1Y Venom
- Eurocopter AS365 Dauphin / Harbin Z-9
- Eurocopter AS565 Panther
- Sikorsky S-76
- Sikorsky UH-60 Black Hawk
- TAI T625 Gökbey
Related lists
References
Sources
External links
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