Engineering:Caudron C.870
From HandWiki
| C.870 | |
|---|---|
| Role | Trainer |
| Manufacturer | Caudron |
| First flight | January 1940 |
| Number built | 2 |
The Caudron C.870 was a training aircraft built by Caudron in the early 1940s.
It was a low-wing monoplane of all-metal construction. Although two prototypes were built, the C.870 was not put into series production.
Specifications
Data from [1]
General characteristics
- Crew: 2
- Length: 9.98 m (32 ft 9 in)
- Wingspan: 10.2 m (33 ft 6 in)
- Wing area: 16.8 m2 (181 sq ft)
- Powerplant: 1 × Renault 12R-09 V-12 inverted air-cooled piston engine, 270 kW (360 hp)
- Propellers: 3-bladed constant-speed propeller
Performance
- Maximum speed: 400 km/h (250 mph, 220 kn)
References
- ↑ Parmentier, Bruno. "Caudron C.870" (in fr). Paris. https://www.aviafrance.com/aviafrance1.php?ID=390&ID_CONSTRUCTEUR=313&ANNEE=0&ID_MISSION=0&MOTCLEF=. Retrieved 29 January 2019.
Further reading
- Hauet, Andre (2001). Les avions Caudron :Tome 2. Lela Presse. ISBN 9782914017091.
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