Ka-62
Ka-62
Civil Helicopters
Basic Information
Name
Ka-62
Designation
Ka-62
Alternate Designation
—
Equipment Type
Civil Helicopters
Manufacturer
Russian Helicopters, Kamov
Date of Introduction
2027
Description
The Ka-62 is a civil version of the Ka-60 military assault/transport helicopter developed by Kamov. It retains the single five-bladed main rotor, a 11-bladed tail rotor and wide side doors from the Ka-60. The Ka-62 is powered by two NPO Saturn RD-600V turboshaft engines. The helicopter's cabin can accommodate up to 16 passengers including two pilots. Overall, results slightly lighter and has greater range and better flight performance than the Ka-60.
Air & Air Defense Specifications
Crew
2
Max Speed
310.0 km/h
Range
700.0 km
Service Ceiling
5500 m
Overview (Deagel)
Group
Civil Helicopters
Status
Under Development
Origin
Russia
Contractors
Russian Helicopters*, Kamov
Initial Operational Capability (IOC)
2027
First Flight
April 28, 2016
Total Production
15
Specifications (Deagel)
Crew
2
Main Rotor Blades
5
Passengers
13
Mass — Cargo Hook Capacity
2,500 kilogram
Mass — Max Takeoff Weight
6,800 kilogram
Mass — Payload
2,000 kilogram
Performance — Ceiling
5,500 meter
Performance — Hovering Ceiling
3,000 meter
Performance — Max Range
700 kilometer
Speed — Cruise Speed
270 kph
Speed — Top Speed at High Altitude
310 kph
Gear (Deagel)
Item 1
Turboshaft Engines: Ardiden 3G (2)
Item 2
Turboshaft Engines: RD-600V (2)
Item 3
Turboshaft Engines: VK-1500VM (2)
Item 4
Turboshaft Engines: VK-1600V (2)
Variants
Variant 1
Ka-60 Kasatka
Variant 2
Ka-62
Details
Country of Origin
Russia
Category
Rotary Wing Aircraft
Air > Rotary Wing Aircraft
Sources
deagel.com: https://www.deagel.com/x/x/a000360
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
—
Width
—
Height
—
Weight
6800 kg
Related Equipment (1)
Variant of
Operators (3)
Russia
Brazil
Colombia
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