Mitsubishi SH-60K
License-built anti-submarine patrol version for the Japan Maritime Self-Defense Force (JMSDF).
Overview
Data on design, manufacture and statusDesign authority: Sikorsky Aircraft Corp.
Primary manufacturer: Mitsubishi Heavy Industries Ltd.
Parent type: Sikorsky S-70/H-60
Aircraft status: Operational
Configuration
Primary flight and mechanical characteristicsVTOL 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)
Layout and Dimensions
Data on aircraft size| Overall Dimensions | ||
|---|---|---|
| Overall Height: | ||
| Overall Length: | ||
| Overall Width: | ||
| Airframe Dimensions | ||
|---|---|---|
| Airframe Length: | ||
| Airframe Width: | ||
| Airframe Height: | ||
| 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): | 10,886 kg | 24,000 lb |
| Max Gross Weight (airborne): | ||
| Max Take-off Weight: | 10,886 kg | 24,000 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: | ||
| Never Exceed Speed: | ||
| Service Ceiling: | ||
| Range and Endurance | ||
|---|---|---|
| Max Range: | ||
| Max Endurance: | ||
Engine Details
Aircraft powerplant (lift and/or propulsion)Provided powerplant data is for uninstalled, sea level, static operations.
| Powerplant | ||
|---|---|---|
| Number of engines: | 2 | |
| 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 rotorsDesigned by Mitsubishi.
| Main Rotor Characteristics | ||
|---|---|---|
| Diameter: | 16.40 m | 53.81 ft |
| RPM: | ||
| Direction of Rotation: | Counterclockwise | |
| Hub Type: | ||
| Main Rotor Blade Characteristics | ||
|---|---|---|
| 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 | ||
|---|---|---|
| Disc Area: | 211.24 m² | 2273.9 ft² |
| Disc Loading: | 51.53 kg/m² | 10.555 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: | 4 | |
| Blade Construction: | ||
| Blade Chord: | ||
| Blade Twist: | ||
| Tail Rotor Derived Characteristics | ||
|---|---|---|
| Disc Area: | ||
| Solidity: | ||
| Tail Rotor Blade Derived Characteristics | ||
|---|---|---|
| Tip Speed: | ||
| Blade Area (per blade): | ||
Related VFS Resources
Resources related to the SH-60K , provided by the Vertical Flight Society.Forum Proceedings
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Related Public Resources
Resources related to the SH-60K , provided by public sources across the internet.Publicly-funded resources provided by the US Government
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Public resources provided by select scholarly and academic sources
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