First helicopter of Landgraf Helicopter Corporation developed in 1944.  Bought by the USAF for testing in 1948; however, the aircraft crashed in the testing and the pilot was killed.  The project was halted following the incident.

Overview

Data on design, manufacture and status

Design authority: Landgraf Helicopter Corporation

Primary manufacturer: Landgraf Helicopter Corporation

Parent type: No type defined

Aircraft status: No longer flying

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Tandem (Lateral) (x2)

Crew required: 1

Crew seating: Single seater

Landing gear: Wheels (non-retractable)

Overall Dimensions

Data on aircraft size

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 1

Engine designation: Pobjoy R reciprocating

Engine manufacturer: Pobjoy Motors and Aircraft

Take-off / rated power: 63 kW (85 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 386 kg (850 lb)

Max Range: 187 km (101 nm)

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