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Brock KB-3
The Brock KB-3 is an American autogyro that was designed by Ken Brock, produced by Ken Brock Mfg and introduced in 1985. The aircraft was supplied as a kit for amateur construction and was also available as plans.〔Cliche, Andre: ''Ultralight Aircraft Shopper's Guide'' 8th Edition, page F-3. Cybair Limited Publishing, 2001. ISBN 0-9680628-1-4〕〔Downey, Julia: ''2005 Trikes 'Chutes and Rotorcraft Directory'', Kitplanes, Volume 22, Number 2, February 2005, page 57. Belvoir Publications. ISSN 0891-1851〕
==Design and development==
The KB-3 was derived from the 1970 KB-2 and specifically designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of . The aircraft has a standard empty weight of . It features a single main rotor, a single-seat open cockpit without a windshield, tricycle landing gear and a twin cylinder, liquid-cooled, two-stroke, dual-ignition Rotax 582 engine in pusher configuration.〔
The aircraft fuselage is made from bolted-together aluminum tubing. Its diameter rotor has two blades. Factory available options included a main rotor pre-rotator, a rotor brake and an instrument package. Fuel capacity is and is housed in a combination pilot seat/fuel tank.〔
Due to its small size and light weight the KB-3 is easy to transport by trailer and can be set up to fly in ten minutes.〔
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