Lockheed CL-475

The Lockheed CL-475 is a two-seat, single-engine light helicopter developed by Lockheed to explore rigid rotor technology.

The CL-475 has a three-bladed main rotor and a two-bladed tail rotor.

Only one was built.

Specifications

Crew

2

Height

9 ft 3 in (2.82 m)

Empty weight

1,625 lb (737 kg)

Gross weight

2,000 lb (907 kg)

Powerplant

1 × Lycoming VO-360-A1A four-cylinder air-cooled piston engine , 140 hp (104 kW)

Main rotor diameter

32 ft 0 in (9.75 m)

Performance

Maximum speed

90 mph (145 km/h, 78 kn)

Range

75 mi (120 km, 65 nmi)

Service ceiling

2,000 ft (610 m).

 

 

 

 

 

 

Share on facebook