Overview

Data on design, manufacture and status

Design authority: University of Maryland

Primary manufacturer: University of Maryland

Parent type: No type defined

Aircraft status: In development

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Multi-rotor (x4)

Crew required: 1

Crew seating: Single seater

Landing gear: Other

Overall Dimensions

Data on aircraft size

Overall Length: 30.50 m (100.1 ft)

Overall Width: 30.50 m (100.1 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 4

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 103 kg (226 lb)

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Related Public Resources

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