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Brock KB 3

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Manufacturer
  
Ken Brock Manufacturing

Brock KB-3 httpsuploadwikimediaorgwikipediacommonsthu

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.

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.

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.

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.

Specifications (KB-3)

Data from Cliche and Kitplanes

General characteristics

  • Crew: one
  • Length: 12 ft 0 in (3.66 m)
  • Empty weight: 250 lb (113 kg)
  • Gross weight: 600 lb (272 kg)
  • Fuel capacity: 5 U.S. gallons (19 L; 4.2 imp gal)
  • Powerplant: 1 × Rotax 582 twin cylinder, liquid-cooled, two-stroke dual-ignition aircraft engine, 64 hp (48 kW)
  • Main rotor diameter: × 22 ft 0 in (6.71 m)
  • Main rotor area: 380 sq ft (35 m2)
  • Performance

  • Maximum speed: 63 mph (101 km/h; 55 kn)
  • Cruise speed: 60 mph (52 kn; 97 km/h)
  • Range: 100 mi (87 nmi; 161 km)
  • Service ceiling: 10,000 ft (3,048 m)
  • Rate of climb: 1,200 ft/min (6.1 m/s)
  • Disk loading: 1.58 lb/sq ft (7.7 kg/m2)
  • References

    Brock KB-3 Wikipedia


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