Caudron Simoun
Specifications for C.630 from Wikipedia
General characteristics
Crew: 1-2: pilot and (optional) co-pilot
Capacity: 2 passengers
Length: 9.10 m (29 ft 10 in)
Wingspan: 10.4 m (34 ft 2 in)
Height: 2.3 m (7 ft 7 in)
Wing area: 16 m² (170 ft²)
Empty weight: 755 kg (1,660 lb)
Max takeoff weight: 1,380 kg (3,040 lb)
Powerplant: 1× Renault Bengali 6Q-09 six-cylinder inline engine, 220 hp (160 kW)
Performance
Maximum speed: 300 km/h (160 knots, 190 mph)
Range: 1,500 km (810 nm, 930 mi)
Service ceiling: 6,000 m (20,000 ft)
Variants
- C.500 Simoun I - experimental, one built.
- C.520 Simoun - experimental, one built.
- C.620 Simoun IV - experimental, one built.
- C.630 Simoun - initial production version with Renault Bengali 6Pri engine, 20 built.
- C.631 Simoun - modified version with a Renault Bengali 6Q-01 engine, three built.
- C.632 Simoun - similar to C.631, one built.
- C.633 Simoun - modified fuselage with a Renault Bengali 6Q-07 engine, 6 built.
- C.634 Simoun - modified wing and take-off weight with either a Renault Bengali 6Q-01 or Renault Bengali 6Q-09 engine, 3 built.
- C.635 Simoun - improved cabin layout and either a Renault Bengali 6Q-01 or Renault Bengali 6Q-09 engine, 46 built and conversions from earlier versions.
- C.635M Simoun - military version with either a Renault Bengali 6Q-09 or Renault Bengali 6Q-19 engine, 489 built.