| C.570 Kangourou | |
|---|---|
| General information | |
| Type | Bomber/military transport |
| National origin | France |
| Manufacturer | Caudron-Renault |
| Number built | 1 |
| History | |
| First flight | 24 November 1935 |
TheCaudron C.570 was a French twin-engine aircraft designed and built byCaudron in the mid-1930s. It was designed to function in multiple roles; as a bomber, passenger transport, paratroop aircraft, cargo aircraft and air ambulance.
The Caudron C.570 was primarily designed to fill a gap in the types of aircraft available to French armed forces, that of a troop-carrier, though it could take on other roles. It was alow wingcantilevermonoplane with wings in three parts, a 7.80 m (25 ft 7 in) span rectangular centre section and outertrapezoidal panels, ending in rounded tips. The wings were built around twin boxspars made ofspruce andplywood. The central section had an aluminium frame and light metal skin; the outer panels were ply-covered. Multi-sectionailerons filled more than half the span of the outer panels'trailing edges.[1]
The C.570 had a square sectionfuselage. Its 7.80 m (25 ft 7 in)-long forward part, reaching aft to the wing trailing edges, housed the crew and up to eighteen troops and was built with aluminiumlongerons and frames, skinned in light alloy. There was a cabin in the nose for a crew-member who acted as navigator, bomb aimer and second pilot and behind that, ahead the engines, a well glazed pilot's cabin with side-by-side seating. Immediately behind the pilot was a cabin for the wireless operator and also four passengers. Next came the main cabin, which seated fourteen men and finally a small cabin for any injured.[1] The distribution of the crew may have depended on the designated role, e.g. transport or bomber, asFlight describes a different arrangement.[2] Access to the forward cabins was via a large port-side door. The main cabin had another large door on the starboard side at the rear; there was also a trapdoor large enough for four parachutists to leave together. The rear part of the fuselage was a weldedchrome-molybdenum steel tube girder,fabric covered over a light wooden frame.[1]
It was powered by two 520 kW (700 hp) water-cooledRenault 18Jbr 18-cylinderW engines, mounted on welded steel tubes in the wing centre section withradiators below them. The C.570'shydraulicallyretractable main undercarriage had wheels onMessieroleo struts which folded backwards behind the engines, giving it a track of 7.80 m (25 ft 7 in).[1]
The C.570 had atwin tail with itstailplane mounted at the top of the fuselage. Together with theelevators it was trapezoidal in plan; the fins were of theendplate type, oval in profile and withrudders split into two sections to allow elevator movement. Both horizontal and vertical control surfaces hadFlettner-typeservo tabs. Below the tail was a fixed tailwheel.[1]
The C.570 flew for the first time, with pilots Delmotte and Lacombe and engineerMarcel Riffard, on 24 November 1935.[3] By July 1936 it was undergoing official tests[4] atVillcaoublay. In November it appeared there amongst an array of prototypes[5] and its prolonged trials were only ended in September 1937, by when it had acquired the nameKangourou.[6]
Data from Les Ailes 26 March 1936[1]
General characteristics
Performance