| CM.8 | |
|---|---|
 | |
| Role | High-performance sailplane |
| Manufacturer | Fouga |
| First flight | June 1949 |
| Variants | Fouga CM.88 Gemeaux |
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 CM.170 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 Turbomeca 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.
Data fromJane's All the World's Aircraft 1951–52 [4]
General characteristics
Performance
Related lists
This is a list of aviation-related events from 1949:
The Fouga CM.170 Magister is a 1950s French two-seat jet trainer aircraft that was developed and manufactured by French aircraft manufacturer Établissements Fouga & Cie. Easily recognizable by its V-tail, almost 1,000 have been built in France and under licence in West Germany, Israel, and Finland.
The Farman F.220 and its derivatives were thick-sectioned, high-winged, four engined French monoplanes from Farman Aviation Works. Based on the push-pull configuration proven by the F.211, design started in August 1925 and the first flight of the prototype was on 26 May 1932. The largest bomber to serve in France between the two world wars was the final F.222 variant. One variation was intended to be an airliner.
The Turbomeca Palas is a diminutive centrifugal flow turbojet engine used to power light aircraft. An enlargement of the Turbomeca Piméné, the Palas was designed in 1950 by the French manufacturer Société Turbomeca, and was also produced under licence by Blackburn and General Aircraft in the United Kingdom and Teledyne Continental Motors in the United States as the Continental Model 320.
The Arsenal O.101 was a French research aircraft that flew shortly after World War II. It was a low-wing monoplane of conventional configuration with fixed tailwheel undercarriage, but incorporated several novel features for its role as an airborne testbed for evaluating airfoil sections and control surface designs. It was designed to accommodate a pilot and an observer in tandem cockpits. However, since the observer was to be watching the aircraft's wings, this cockpit was sunken fully into the fuselage, affording no fore-and-aft view at all. The pilot's cockpit was set well back along the fuselage, near the tail.
The CAB GY-30 Supercab was a two-seat light aircraft built in France in 1954, as a further development of the CAB Minicab. The design was performed by Yves Gardan, a onetime employee of French aeronautical company SIPA. Changes incorporated in the Supercab included a more powerful engine, greater wingspan, manually retractable undercarriage, and slotted flaps that replaced the split flaps of the Minicab.
The Fouga CM.88 Gemeaux was a 1950s French engine test-bed aircraft produced by Fouga. An unusual aircraft, it was two aircraft joined by a common wing.
The Brochet MB.100 was a three-seat light aircraft developed in France in the early 1950s.
The SNCASE SE.3120 Alouette ("Lark") was a utility helicopter developed in France in the early 1950s but which did not enter production. Designed in parallel with the SE.3110, the Alouette shared that machine's dynamic components, with the exception of the SE.3110's unusual twin tail rotor, which was replaced by a single rotor, and the addition of a three-bladed gyroscopic stabiliser under the main rotor (similar to the stabiliser bar used by Bell helicopters. The Alouette featured an open-framework fuselage behind a cockpit that was enclosed by a bubble canopy. Skid undercarriage and tricycle gear were both tested.
Fouga was a French manufacturing company established by Gaston Fouga at Béziers during 1920. Originally specialising in the repair of railway rolling stock, the firm eventually became most noted for the aircraft it produced from its woodworking facilities at Aire-sur-l'Adour.
The SCAN 20 was a 1940s French flying-boat training monoplane designed and built by Société de Constructions Aéro-Navales de Port-Neuf (SCAN). The prototype was built in secret in 1941. It was hidden until the liberation of France and first flown in 1945.
The Pilatus P-4 was a Swiss five-seat cabin monoplane designed and built by Pilatus, but had little sales success.
The SIPA S.200 Minijet was a light sporting jet aircraft designed and produced by the French aircraft manufacturer Société Industrielle Pour l’Aéronautique (SIPA). It is designed to perform liaison, training, and aerobatic flights. The Minijet was claimed to be the first jet-powered light touring aircraft
The Morane-Saulnier MS.755 Fleuret was a prototype French two-seat jet trainer designed and built by Morane-Saulnier. It failed to gain any orders but was developed into the larger four-seat MS.760 Paris.
The Morane-Saulnier MS.1500 Épervier was a 1950s French two-seat ground attack and reconnaissance aircraft. Designed and built by Morane-Saulnier to meet a French Air Force requirement, it did not enter production.
The SIPA S.300 was a French turbojet powered basic trainer, claimed to be the first of its kind anywhere. Only one was built, the prototype crashing after a year's development.
The Bréguet Br 900 Louisette was a short-span, single-seat competition sailplane built in France in the 1940s. It set some French gliding records but was unsuccessful at the international level. Only six production aircraft were built.
The Sud-Est or SNCASE SE-2100, sometimes known as the Satre SE-2100 after its designer, was a tailless, pusher configuration touring monoplane with a single engine and cabin for two. Only one was built.
The SNCASE SE-1210 was an experimental French flying-boat designed and built by SNCASE as a flying scale model of the proposed SE-1200 transatlantic flying boat.
The SNCASO SO.3050 was a two seat light touring aircraft that was designed and built in France towards the end of World War II. Only one was completed and that was soon abandoned.
