A two-seat ultralight helicopter meant for recreational or training flights. This aircraft is unique as it is the only helicopter to feature a ballistic parachute, which is located above the main rotor.

Overview

Data on design, manufacture and status

Design authority: Curti Aerospace

Primary manufacturer: Curti Aerospace

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: Tail rotor

Crew required: 1-2

Crew seating: Side-by-side

Landing gear: Skids

Overall Dimensions

Data on aircraft size

Overall Height: 2.50 m (8.2 ft)

Overall Length: 8.70 m (28.5 ft)

Overall Width: 1.60 m (5.2 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 1

Engine designation: PBS Aerospace TS100 turbine

Engine manufacturer: PBS GROUP, a.s.

Max continuous power: 105 kW (141 hp)

Take-off / rated power: 180 kW (241 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 700 kg (1543 lb)

Max Range: 318 km (172 nm)

Max Endurance: 2.3 hrs (2.3 hrs)

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