Brock KB-3

Last updated

KB-3
Ken Brock KB-3 Gyrocopter (N112SW).jpg
Role Autogyro
National origin United States
Manufacturer Ken Brock Mfg
Designer Ken Brock
Introduction1985
StatusProduction completed
Produced1985-2005
Number built200 (2005)
Developed from Brock KB-2

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. [1] [2]

Contents

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 254 lb (115 kg). The aircraft has a standard empty weight of 250 lb (113 kg). 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 64 hp (48 kW) Rotax 582 engine in pusher configuration. [1]

The aircraft fuselage is made from bolted-together aluminum tubing. Its 22 ft (6.7 m) diameter rotor has two blades. Factory available options included a main rotor pre-rotator, a rotor brake and an instrument package. Fuel capacity is 5 U.S. gallons (19 L; 4.2 imp gal) and is housed in a combination pilot seat/fuel tank. [1]

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. [1]

Specifications (KB-3)

Data from Cliche and Kitplanes [1] [2]

General characteristics

Performance

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References

  1. 1 2 3 4 5 Cliche, Andre: Ultralight Aircraft Shopper's Guide 8th Edition, page F-3. Cybair Limited Publishing, 2001. ISBN   0-9680628-1-4
  2. 1 2 Downey, Julia: 2005 Trikes 'Chutes and Rotorcraft Directory, Kitplanes, Volume 22, Number 2, February 2005, page 57. Belvoir Publications. ISSN 0891-1851