The Ka-62 is a multipurpose helicopter with maximum internal and slung payloads of 2000 and 2500 kg, respectively.  The cabin can carry up to 16 passengers in addition to the pilots.

Overview

Data on design, manufacture and status

Design authority: Kamov Design Bureau

Primary manufacturer: Kamov

Parent type: No type defined

Aircraft status: In development

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Single main rotor

Dedicated control device: Fenestron/Shrouded tail rotor

Crew required: 1-2

Crew seating: Side-by-side

Landing gear: Wheels (all retractable)

Layout and Dimensions

Data on aircraft size

Overall Dimensions
Overall Height:  
Overall Length:  
Overall Width: 13.80 m 45.3 ft
Airframe Dimensions
Airframe Length: 13.50 m 44.3 ft
Airframe Width: 2.76 m 9.1 ft
Airframe Height: 4.87 m 16.0 ft
Landing Gear Dimensions
Landing Gear Base: 5.47 m 17.9 ft
Landing Gear Track:  
Cabin Dimensions
Cabin Internal Height: 1.30 m 4.3 ft
Cabin Internal Length: 4.10 m 13.5 ft
Cabin Internal Width: 1.74 m 5.7 ft

Weights and Performance

Data on aircraft weight and flight characteristics

Weights
Max Gross Weight (ground): 6,500 kg 14,330 lb
Max Gross Weight (airborne):  
Max Take-off Weight: 6,500 kg 14,330 lb
Empty Weight:  
Useful Load:  
Empty Weight Fraction:  
Climb Performance
Max Rate of Climb: 14 m/s 2,756 fpm
Hover Performance
Hover Ceiling IGE: 3,800 m 12,467 ft
Hover Ceiling OGE: 3,300 m 10,827 ft
Limitations
Max Level Flight Speed: 308 km/h 166 kts
Never Exceed Speed:  
Service Ceiling: 5,700 m 18,701 ft
Range and Endurance
Max Range: 770 km 416 nm
Max Endurance: 4 hrs 4 hrs

Engine Details

Aircraft powerplant (lift and/or propulsion)

Provided powerplant data is for uninstalled, sea level, static operations.

Powerplant
Number of engines: 2
Designation: Turbomeca Ardiden 3G turbine
Manufacturer: Turbomeca
Normal Ratings
Max continuous:  
Take-off / rated:  
Intermediate:  
Maximum:  
OEI Ratings
OEI contingency:  
OEI continuous:  
OEI 30-second:  
OEI intermediate:  

Primary Lift Device

Data on primary lift devices such as main rotors

Main Rotor Characteristics
Diameter: 13.80 m 45.28 ft
RPM:  
Direction of Rotation: Clockwise
Hub Type:
Main Rotor Blade Characteristics
Blade Construction:
Blade Chord:  
Blade Tip Geometry: Swept/anhedral
Blade Twist:  
Number of Blades: 5
Main Rotor Derived Characteristics
Disc Area: 149.57 m² 1610.0 ft²
Disc Loading: 43.46 kg/m² 8.901 lb/ft²
Solidity:  
Main Rotor Blade Derived Characteristics
Blade area per blade:  
Tip Speed:  

Primary Control Device

Data on primary control devices such as tail rotors

Tail Rotor Characteristics
Diameter:  
Configuration: Unblocked
Direction of Rotation: Top blade aft
RPM:  
Tail Rotor Blade Characteristics
Number of Blades: 10
Blade Construction:  
Blade Chord:  
Blade Twist:  
Tail Rotor Derived Characteristics
Disc Area:  
Solidity:  
Tail Rotor Blade Derived Characteristics
Tip Speed:  
Blade Area (per blade):  

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