Audenis C2
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| C2 | |
|---|---|
| General information | |
| Type | Trainer |
| National origin | France |
| Designer | |
| Number built | 1 |
| History | |
| First flight | 1916 |
The Audenis C2 was a two-seat fighter biplane, designed and built in France during 1916. Probably powered by a 130 hp (97 kW) Clerget 9B 9-cylinder rotary engine, the C2 had equal span single bay biplane wings with the lower mainplane set well below the fuselage attached by the rear undercarriage struts and a pair of struts at the leading edge. The undercarriage was of conventional tailskid configuration with the mainwheel axle attached to the fuselage by V-struts. Pilot and gunner were seated in individual cockpits with the pilot under the centre-section and the gunner aft of the wings, provided with a single fixed Vickers machine-gun fired by the pilot and a machine-gun on a ring in the rear cockpit. Development of the C2 did not continue after initial flight trials.[1]