A modification of the Ka-10, the Ka-15 has a closed fuselage.  The aircraft may be equipped with floats for landing gear.  NATO Designation of the helicopter is Hen.  The cabin can seat a single passenger in additon to the pilot.

Overview

Data on design, manufacture and status

Design authority: Kamov Design Bureau

Primary manufacturer: Kamov

Parent type: Kamov Ka-15

Aircraft status: No longer flying

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Coaxial (x2)

Crew required: 1

Crew seating: Single seater

Landing gear: Wheels (non-retractable)

Layout and Dimensions

Data on aircraft size

Overall Dimensions
Overall Height: 3.35 m 11.0 ft
Overall Length: 9.96 m 32.7 ft
Overall Width: 9.96 m 32.7 ft
Airframe Dimensions
Airframe Length: 6.26 m 20.5 ft
Airframe Width: 2.85 m 9.4 ft
Airframe Height: 3.35 m 11.0 ft
Landing Gear Dimensions
Landing Gear Base:  
Landing Gear Track:  
Cabin Dimensions
Cabin Internal Height:  
Cabin Internal Length:  
Cabin Internal Width:  

Weights and Performance

Data on aircraft weight and flight characteristics

Weights
Max Gross Weight (ground): 1,370 kg 3,020 lb
Max Gross Weight (airborne):  
Max Take-off Weight: 1,370 kg 3,020 lb
Empty Weight:  
Useful Load:  
Empty Weight Fraction:  
Climb Performance
Max Rate of Climb:  
Hover Performance
Hover Ceiling IGE:  
Hover Ceiling OGE:  
Limitations
Max Level Flight Speed: 155 km/h 84 kts
Never Exceed Speed:  
Service Ceiling: 3,500 m 11,483 ft
Range and Endurance
Max Range: 350 km 189 nm
Max Endurance:  

Engine Details

Aircraft powerplant (lift and/or propulsion)

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

Powerplant
Number of engines: 1
Designation: Ivchenko AI-14V reciprocating
Manufacturer: Ivchenko
Normal Ratings
Max continuous:  
Take-off / rated: 188 kW 252 hp
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: 9.96 m 32.68 ft
RPM:  
Direction of Rotation: Counter-rotating
Hub Type: Coaxial
Main Rotor Blade Characteristics
Blade Construction:
Blade Chord:  
Blade Tip Geometry: Conventional
Blade Twist:  
Number of Blades: 3
Main Rotor Derived Characteristics
Disc Area: 77.91 m² 838.7 ft²
Disc Loading: 8.79 kg/m² 1.801 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: Unknown
Direction of Rotation: Unknown
RPM:  
Tail Rotor Blade Characteristics
Number of Blades:  
Blade Construction: N/A
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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Related Public Resources

Resources related to the Ka-15 , provided by public sources across the internet.

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