This is the aircraft in a 4 main blade configuration with auxiliary jet propulsion (1xP&W J-60-P2) mounted on the port side.

 

Overview

Data on design, manufacture and status

Design authority: Lockheed-California Company

Primary manufacturer: Lockheed-California Company

Aircraft status: No longer flying

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Compound type: Lift and Thrust

Lift configuration: Coaxial

Dedicated control device: Tail rotor

Dedicated propulsion devices: 1

Crew required: 1

Crew seating: Side-by-side

Landing gear: Skids (retractable)

Overall Dimensions

Data on aircraft size

Overall Width: 10.67 m (35.0 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 1

Engine designation: UAC PT6B-9 turbine

Engine manufacturer: United Aircraft of Canada

Take-off / rated power: 410 kW (550 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 2359 kg (5200 lb)

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