License-built anti-submarine patrol version for the Japan Maritime Self-Defense Force (JMSDF).
Design authority: Sikorsky Aircraft Corp.
Primary manufacturer: Mitsubishi Heavy Industries Ltd.
Parent type: Sikorsky S-70/H-60
Aircraft status: Operational
VTOL type: Helicopter
Lift configuration: Single main rotor
Dedicated control device: Tail rotor
Crew required: 2
Crew seating: Side-by-side
Landing gear: Wheels (non-retractable)
Overall Dimensions | ||
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Airframe Dimensions | ||
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Landing Gear Dimensions | ||
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Cabin Dimensions | ||
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Weights | ||
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Max Gross Weight (ground): | 10,886 kg | 24,000 lb |
Max Gross Weight (airborne): | ||
Max Take-off Weight: | 10,886 kg | 24,000 lb |
Empty Weight: | ||
Useful Load: | ||
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Climb Performance | ||
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Limitations | ||
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Service Ceiling: |
Range and Endurance | ||
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Provided powerplant data is for uninstalled, sea level, static operations.
Powerplant | ||
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Number of engines: | 2 |
Normal Ratings | ||
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Intermediate: | ||
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OEI Ratings | ||
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OEI continuous: | ||
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Designed by Mitsubishi.
Main Rotor Characteristics | ||
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Diameter: | 16.40 m | 53.81 ft |
RPM: | ||
Direction of Rotation: | Counterclockwise | |
Hub Type: |
Main Rotor Blade Characteristics | ||
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Blade Construction: | Composite spar and skins with honeycomb core and titanium/nickel leading edge shield | |
Blade Chord: | ||
Blade Tip Geometry: | Dihedral with swept anhedral | |
Blade Twist: | ||
Number of Blades: | 4 |
Main Rotor Derived Characteristics | ||
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Disc Area: | 211.24 m² | 2273.9 ft² |
Disc Loading: | 51.53 kg/m² | 10.555 lb/ft² |
Solidity: |
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Tail Rotor Characteristics | ||
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Diameter: | ||
Configuration: | Unknown | |
Direction of Rotation: | Unknown | |
RPM: |
Tail Rotor Blade Characteristics | ||
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Number of Blades: | 4 | |
Blade Construction: | ||
Blade Chord: | ||
Blade Twist: |
Tail Rotor Derived Characteristics | ||
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Disc Area: | ||
Solidity: |
Tail Rotor Blade Derived Characteristics | ||
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Tip Speed: | ||
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