Lockheed CL-475

The Lockheed CL-475 (registration N6940C) is a two-place 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.

Made by Lockheed Corporation.

Empty Weight Lb
1625
Designer
Irven Culver
Eng 1 Type
Lycoming VO-360-A1A four-cylinder air-cooled piston engine
Max Speed Mph
90
Lists
* List of rotorcraft
Eng 1 Kw
104
Status
On display
Gross Weight Lb
2000
Number Built
1
Crew
2
Empty Weight Kg
737
Gross Weight Kg
907
Height In
3
Rot Number
1
Range Km
120
Manufacturer
Lockheed Corporation
Rot Dia Ft
32
Ceiling Ft
2000
First Flight
2
Max Speed Kmh
145
Height Ft
9
National Origin
United States
Category
Helicopters
Lockheed aircraft
United States experimental aircraft 1950-1959
Met Or Eng
eng
Rot Dia In
Height M
3
Ceiling M
610
Eng 1 Hp
140
Eng 1 Number
1
Related
* Lockheed XH-51
Rot Dia M
10
Range Miles
75

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