CSIR Experimental Autogyro II
| 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
Bibliography
- Taylor, ed. (1973). Jane's All the World's Aircraft 1973-74. London, United Kingdom: Jane's Yearbooks. ISBN 0-354-00117-5.
|first1=missing|last1=in Authors list (help)
| ||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||