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KAMOV
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KA-25 |

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ASW helicopter with a short, stubby fuselage and
contrarotating, coaxial rotors. The contra-rotating rotors eliminated the need for an
anti-torque tail rotor, and made a very compact design possible, with obvious benefits for
shipboard operations.
Modifications: |
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Characteristics |
Information |
Characteristics |
Information |
| First
Flight Primer Vuelo |
1961 |
Engine Motor |
2
Glushenko |
| Seating
Capacity Plazas |
2 / 12 |
Power Potencia |
990 HP |
| Empty
Weight Peso Vacío |
NA |
Hover
Ceiling O.G.E. Estacionario O.G.E |
NA |
| Maximum
Weight Peso Máximo |
NA |
Hover
Ceiling I.G.E. Estacionario I.G.E |
NA |
| Vel.
Cruise Vel. crucero |
105 Kts |
Service
Ceiling Techo de Servicio |
NA |
| V.N.E. V.N.E |
118 Kts |
Maximum
Range (Std) Alcance (Std) |
350 NM |
Copyright © 1999 / 2003