Caudron G.4
Bomber / Reconnaissance Biplane
The Caudron G.4 is a twin-engined two-seat reconnaissance and bomber biplane aircraft produced by the French manufacturer Société des avions Caudron.
Crew | 2 |
Propulsion | 2 Rotary Engines | |
Engine Model | Le Rhône 9C | |
Engine Power (each) | 60 kW | 80 hp |
Speed | 131 km/h | 71 kts 82 mph |
Service Ceiling | 4.300 m | 14.108 ft |
Range | 400 km | 216 NM 249 mi. |
Empty Weight | 500 kg | 1.102 lbs |
max. Takeoff Weight | 1.330 kg | 2.932 lbs |
Wing Span | 17,20 m | 56 ft 5 in |
Wing Area | 36,8 m² | 396 ft² |
Length | 7,27 m | 23 ft 10 in |
Height | 2,60 m | 8 ft 6 in |
First Flight | 03/1915 | |
Production Status | out of production | |
Total Production | 1421 | |
Developed from | Caudron G.3 |
Data for (Version) | Caudron G.4 |
[Photo-ID: 10240] © Karsten Palt 2014-05-28 | |
![]() | Caudron G.4 French Air Force / Armee de l Air Reg.: C4263 |
NASM Udvar Hazy Center [Chantilly, VA] |
[Photo-ID: 10241] © Karsten Palt 2014-05-28 | |
![]() | Caudron G.4 French Air Force / Armee de l Air Reg.: C4263 |
NASM Udvar Hazy Center [Chantilly, VA] |