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Caudron G.VI

Posted on April 25, 2026 By

In the autumn of 1915, Gaston Caudron set out to correct the shortcomings of the R.4, but in December, the talented designer died in an aviation accident. His brother René continued the work, resulting in the Caudron G.VI. This aircraft was very similar to the R.4 in construction and appearance, but significantly smaller in size and mass.

The machine evolved from a three-strut biplane into a two-strut sesquiplane. It was equipped with light “Rhône” rotary engines, typically used on fighters, and its crew was reduced from three people to two.

Table of Contents

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    • Development and Innovative Design
    • Combat Performance
    • Production and Obsolescence
    • Technical Specifications
  • Image gallery of the Caudron G.VI
    • How to cite this article:

Development and Innovative Design

The prototype’s first flight took place in June 1916. The flight characteristics of the lightened Caudron significantly improved, with a particularly sharp increase in climb rate, though for a bomber this indicator was not considered paramount. The bomb load remained quite low.

However, unlike the practically defenseless Farmans and Voisins, the G.6 could operate effectively during the day. This gave it a significant tactical advantage in daytime operations of the era.

Combat Performance

In the summer of 1916, the G.6 was adopted and mass-produced. However, by the spring of that same year, the French industry had already mastered the production of new aircraft engines with over 200 hp. From then on, bombers equipped with weaker engines quickly became obsolete.

A total of 512 Caudron G.6 aircraft were built. Despite its short frontline operational lifespan, the G.VI represented an important step in the evolution of French World War I bombers.

Production and Obsolescence

Technical Specifications

Modification G.VI
Wingspan, m 17.22
Length, m 8.60
Wing area, m2 39.00
Empty weight 940
Normal takeoff weight 1440
Engine type 2 Piston engine Gnome Rhone
Power, hp 2 x 110-130
Maximum speed, km/h 145
Cruising speed, km/h 122
Practical range, km 275
Rate of climb, m/min 267
Service ceiling, m 4400
Crew, crew members 3
Armament one machine gun turret with a 7.7-mm Lewis machine gun, up to 100 kg of bombs

Image gallery of the Caudron G.VI

How to cite this article:

APA: Caudron G.VI (). Caudron G.VI. archivoaereo.com. https://archivoaereo.com/en/caudron-g-vi-2/
VANCOUVER: Caudron G.VI [online]. archivoaereo.com; [cited 2026-04-26]. Available at: https://archivoaereo.com/en/caudron-g-vi-2/
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