The fourteen-seater military transport aircraft Caudron C.570 (CR.570) Kangourou was completed in the autumn of 1935. It was a wooden low-wing monoplane, equipped with two Renault 18Jbr engines, each producing 700 hp. Its maiden flight took place on November 24, 1935.
Design and Technical Specifications
During tests, the aircraft displayed promising characteristics. However, the project did not progress beyond the construction of the prototype. The C.570 remained a single example and, according to some reports, saw limited use by the French Air Force.
Development and Operational Legacy
Technical Specifications
| Modification | C. 570 |
| Wingspan, m | 28.88 |
| Length, m | 19.36 |
| Height, m | 4.60 |
| Wing area, m2 | 110.00 |
| Empty weight | 5860 |
| Normal takeoff weight | 10100 |
| Engine type | 2 Piston engine Renault 18Jbr |
| Power, hp | 2 x 700 |
| Maximum speed, km/h | 276 |
| Cruising speed, km/h | 245 |
| Practical range, km | 1280 |
| Practical ceiling, m | 5000 |
| Crew, crew members | 2 |
| Payload | up to 12 passengers |
Image and diagram gallery of the Caudron C.570 (CR.570) Kangourou
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VANCOUVER: Caudron C.570 (CR.570) Kangourou [online]. wp.archivoaereo.com; [cited 2026-06-21]. Available at: https://wp.archivoaereo.com/en/caudron-c-570-cr-570-kangourou-2/