Fouga CM.8
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| CM.8 | |
|---|---|
| Type | High-performance sailplane |
| Manufacturer | Fouga |
| Designed by | Robert Castello |
| Maiden flight | June 1949 |
The Fouga CM.8 or Castel-Mauboussin CM.8 was a French sailplane of the 1950s, most notable in retrospect due to its place in the development of the Fouga Magister jet trainer. The CM.8 was a single-seat aircraft of conventional sailplane design and designed for aerobatics. Two prototypes were built: the CM.8/13, with a 13-metre wingspan and a conventional empennage, and the CM.8/15 with a 15-metre wingspan and a V-tail.
The pleasing performance of these aircraft led to experiments with mounting a small turbojet on the dorsal fuselage, exhausting between the tail fins. The first of these flew on 14 July 1949, powered by a Turboméca Piméné. Designated the CM.8R this combined the 13-metre wing of the CM.8/13 with the tail of the CM.8/15. Two examples were built, and as experiments progressed in the 1950s, they were fitted with increasingly powerful engines, and increasingly shorter wingspans. A twin-fuselage example was also built as the CM.88 as an engine testbed
[edit] Specifications (CM.8/13)
General characteristics
- Crew: One pilot
- Length: 6.55 m (21 ft 6 in)
- Wingspan: 13.00 m (42 ft 8 in)
- Height: 1.95 m (6 ft 5 in)
- Wing area: 13 m² (140 ft²)
- Aspect ratio: 13
- Empty weight: 247 kg (545 lb)
- Gross weight: 330 kg (728 lb)
Performance
- Rate of sink: 1.1 m/s (216 ft/min)
[edit] References
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions, 239.
- Planeurs et Avions
[edit] See also
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