CSIR Experimental Autogyro II

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Experimental Autogyro II
Role Two-seat experimental autogyro
National origin South Africa
Manufacturer Council for Scientific and Industrial Research
First flight 30 November 1972
Number built 1

The CSIR Experimental Autogyro II is a South African two-seat experimental autogyro designed and built by the Aeronautics Research Unit of the Council for Scientific and Industrial Research.[1]

Development

As part of the support to South African aircraft manufacturing industry the ARU developed a single-seat autogyro as a research vehicle.[1] Design of the autogyro was started in 1965 and construction followed in April 1967, by 1972 the autogyro, registered ZS-UGL, was ready for tethered tests mounted on a lorry-platform, it made its first free flight on 30 November 1972 at Swartkop Air Force Base.[1] Following the test flights the autogyro was modified.[1]

Design

The autogyro had a box-like fuselage structure made from light-alloy and was fitted with twin fins and rudders with a fixed incidence tailplane mounted between them.[1] It was fitted with a two-bladed teetering rotor, the rotor could be spun up using a shaft drive through a clutch from the engine.[1] The engine located at the rear was a 180 hp (134 kW) Continental O-360-A air-cooled engine driving a two-bladed constant-speed pusher propeller.[1] The crew sat side by side in the enclosed fuselage with dual controls, entrance is through a forward-opening glazed door on each side.[1] The landing gear was a fixed tricycle type with a self-centering and steerable nosewheel.[1]

Specifications

Data from Jane's All the World's Aircraft 1973-74[1]

General characteristics

  • Crew: 2
  • Length: 4.65 m (15 ft 3 in)
  • Main rotor diameter: 11.13 m (36 ft 6¼ in)
  • Width: 1.20 m (3 ft 11¼ in)
  • Height: 2.80 m (9 ft 2¼ in)
  • Main rotor area: 97.20 m2 (1046.25 ft2)
  • Gross weight: 840 kg (1851 lb)
  • Powerplant: 1 × Continental O-360-A four-cylinder, horizontally opposed, air-cooled piston engine, 134 kW (180 hp)

Performance

  • Maximum speed: 154 km/h (96 mph)
  • Cruising speed: 138 km/h (86 mph)
  • Service ceiling: 4267 m (14000 ft)

See also

Related lists

References

Notes

  1. 1.0 1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 Taylor 1973, pp. 174-175

Bibliography

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