The Caudron C.640 Typhon was a 1930s French high-speed single-seat monoplane utility aircraft built by Caudron-Renault.
Contents
History
Similar in concept to the de Havilland DH.88 Comet the Typhon (en: Typhoon) was designed by Georges Otfinovsky and Marcel Riffard for use on long-range postal routes. The first aircraft first flew on 17 June 1935. The aircraft was a twin-engined low-wing cantilever monoplane of wooden construction. Seven C.640s were built. The Typhon established 5000 km speed records. It was not a success in operation as its flexible wings experienced buffeting and vibration problems.
Variants
C.640 Typhon - production model with Renault 6Q engines, 7 built.
C.641 Typhon - record breaking version with raised canopy and increased fuel capacity, 2 built.
C.670 Typhon - prototype high-speed bomber version with a crew of three, similar to the C.640 but with increased dimensions and weights, one built.
Operators
France
French Air Force
Romania
Romanian Air Force
Specifications (C.640)
Data from Aviafrance : Caudron C.640 'Typhon'General characteristics
Crew: 2
Length: 10.95 m (35 ft 11 in)
Wingspan: 11.5 m (37 ft 9 in)
Height: 3 m (9 ft 10 in)
Wing area: 28 m2 (300 sq ft)
Empty weight: 1,630 kg (3,594 lb)
Gross weight: 3,400 kg (7,496 lb)
Powerplant: 2 × Renault 6Q 6-cylinder inverted air-cooled in-line piston engines, 164 kW (220 hp) each
Propellers: 2-bladed Ratier
Performance
Maximum speed: 400 km/h (250 mph, 220 kn)
Cruise speed: 370 km/h (230 mph, 200 kn)
Range: 3,725 km (2,315 mi, 2,011 nmi)
Service ceiling: 7,000 m (23,000 ft)