T he first Kamov helicopter with 'classical' tail-rotor
layout. Ka-60 is a military transport helicopter, replacement for aging Mi-8.
New machine promises 60% saving in fuel consumption, as well as far superior reliability and maintainability. It is to fulfill
a full spectrum of roles, from training and assault troop transport to all-weather reconnaissance and target designation for
attack helicopters.
| Technical data | ||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Type | Ka-60 | ||||||||||
| Function | Military transport Recce Training | ||||||||||
| Year | 1998 | ||||||||||
| Crew | 2 | ||||||||||
| Engines | 2*1280hp Rybinsk RD-600V turboshaft | ||||||||||
| Length (rotor turning) | 15.6m | ||||||||||
| Fuselage Length | 13.46m | ||||||||||
| Height | 4.2m | ||||||||||
| Width over main wheels | 2.50m | ||||||||||
| Rotor diameter | 4-blade 13.5m | ||||||||||
| Rotor disk area | 143.1m2 | ||||||||||
| Tail rotor diameter | 11-blade 1.2m | ||||||||||
| Max. takeoff weight (no external load) |
6500kg | ||||||||||
| Max. gross weight | 6750kg | ||||||||||
| Maximum Level Speed | 300km/h | ||||||||||
| Cruise Speed | 260...270km/h | ||||||||||
| Landing Speed | 0km/h | ||||||||||
| Landing Roll | 0m | ||||||||||
| Takeoff Roll | 0m | ||||||||||
| Ferry Range | 615km | ||||||||||
| Service Ceiling | 5150m | ||||||||||
| Hovering Ceiling (off ground) | 2100m | ||||||||||
| Hovering Ceiling (in ground) | 2900m | ||||||||||
| Climb | |||||||||||
| at 0m | 10.4m/sec | ||||||||||
| Payload | |||||||||||
| Fuel | 1450l | ||||||||||
| Cabin Length | 3.40m | ||||||||||
| Cabin Width | 1.30m | ||||||||||
| Cabin Height | 1.78m | ||||||||||
| Seats (Maximum) | Up to 16 soldiers | ||||||||||
| Seats (Normal) | assault squad of 11 soldiers | ||||||||||
| Stretchers | 6 plus medical personal | ||||||||||
| Internal load | 2000kg | ||||||||||
| Hook load | 2750kg | ||||||||||
| Armament | |||||||||||
| Assorted | On external pylons | ||||||||||
| Created March 1, 1999
by Alexandre Savine |
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