Cierva C.8V
Developed with Avro in 1925. The aircraft is equipped with a rope rotor starter.
Overview
Data on design, manufacture and statusDesign authority: Cierva Autogiro Company Ltd.
Primary manufacturer: Cierva Autogiro Company Ltd.
Parent type: No type defined
Aircraft status: No longer flying
Configuration
Primary flight and mechanical characteristicsVTOL type: Gyroplane
Compound type: N/A compounded with 1 propulsors
Lift devices: 1 Single main rotor
Dedicated control device: 1 Rudder
Crew required: 1 in Tandem arrangement
Landing gear: Other
Key Characteristics
Data on key physical featuresAircraft Details
Data on aircraft configuration, weights, flight performance and equipmentReferences
References and sources used
The History of the Autogiro (Autogiro Data Sheet)
George Townson
AHS Newsletter, 1961, March 1961 (page 12-13)
Periodical
AHS Newsletter, 1961, March 1961 (page 12-13)
Periodical
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