Initial Design and Development
In 1912, brothers René and Gaston Caudron built a small aircraft, designated Caudron G.II (G.2). This was a two-strut, two-seat biplane, equipped with an 80 hp Gnome engine.
Demonstrations and Military Service
The first example of the aircraft was widely used in demonstration air shows in 1913. Following the outbreak of the First World War, several built examples of this aircraft were transferred to the military and used for reconnaissance and observation of the terrain.
Legacy of the Caudron G.II
Later, based on the G.II, the more mass-produced G.III was created, expanding its impact on military aviation.
Technical Specifications
| Modification | G.II |
| Wingspan, m | 12.10 |
| Length, m | 7.25 |
| Wing area, m2 | 28.00 |
| Empty weight | 400 |
| Normal takeoff weight | 700 |
| Engine type | 1 Piston engine Gnome |
| Power, hp | 1 x 80 |
| Maximum speed, km/h | 106 |
| Cruising speed, km/h | 82 |
| Flight duration, h | 3.5 |
| Crew | 2 |
Image and diagram gallery of the Caudron G.II
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How to cite this article:
APA: Caudron G.II (). Caudron G.II. wp.archivoaereo.com. https://wp.archivoaereo.com/en/caudron-g-ii-2/
VANCOUVER: Caudron G.II [online]. wp.archivoaereo.com; [cited 2026-06-15]. Available at: https://wp.archivoaereo.com/en/caudron-g-ii-2/