First flight 02 October 2014. The fuselage is composed completely of Carbon-Fiber.
Latest or last design authority:
Kopter Group AG
Originally designed by Marenco Swisshelicopter Ltd
Latest or last primary manufacturer:
Kopter Group AG
Originally manufactured by Marenco Swisshelicopter Ltd
Parent type: No type defined
Aircraft status: Status unknown
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: Skids
Overall Dimensions | ||
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Overall Height: | ||
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Airframe Dimensions | ||
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Airframe Length: | ||
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Airframe Height: |
Landing Gear Dimensions | ||
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Landing Gear Base: | ||
Landing Gear Track: |
Cabin Dimensions | ||
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Cabin Internal Height: | ||
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Weights | ||
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Max Gross Weight (ground): | 2,650 kg | 5,842 lb |
Max Gross Weight (airborne): | 2,800 kg | 6,173 lb |
Max Take-off Weight: | 2,650 kg | 5,842 lb |
Empty Weight: | ||
Useful Load: | ||
Empty Weight Fraction: |
Climb Performance | ||
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Max Rate of Climb: |
Hover Performance | ||
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Hover Ceiling IGE: | ||
Hover Ceiling OGE: |
Limitations | ||
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Max Level Flight Speed: | 260 km/h | 140 kts |
Never Exceed Speed: | ||
Service Ceiling: |
Range and Endurance | ||
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Max Range: | ||
Max Endurance: | 5 hrs | 5 hrs |
Provided powerplant data is for uninstalled, sea level, static operations.
Powerplant | ||
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Number of engines: | 1 | |
Designation: | Honeywell HTS900-2 turbine | |
Manufacturer: | Honeywell Aerospace |
Normal Ratings | ||
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Max continuous: | ||
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Intermediate: | ||
Maximum: |
OEI Ratings | ||
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OEI contingency: | ||
OEI continuous: | ||
OEI 30-second: | ||
OEI intermediate: |
Main Rotor Characteristics | ||
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Diameter: | ||
RPM: | ||
Direction of Rotation: | Unknown | |
Hub Type: | Bearingless main rotor system |
Main Rotor Blade Characteristics | ||
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Blade Construction: | Composite | |
Blade Chord: | ||
Blade Tip Geometry: | ||
Blade Twist: | ||
Number of Blades: | 5 |
Main Rotor Derived Characteristics | ||
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Disc Area: | ||
Disc Loading: | ||
Solidity: |
Main Rotor Blade Derived Characteristics | ||
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Tip Speed: |
Tail Rotor Characteristics | ||
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Diameter: | ||
Configuration: | Unblocked | |
Direction of Rotation: | Unknown | |
RPM: |
Tail Rotor Blade Characteristics | ||
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Number of Blades: | 10 | |
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: | ||
Blade Area (per blade): |