Audenis C2
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]
Specifications
General Characteristics
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- Wingspan 33.7ft (10.3m)
- Length 24.4ft (7.4m)
- Height 10.2ft (3.1m)
- Empty Weight 5,128lbs (2,326kg)
- Loaded Weight 6,740lbs (3,057kg)
Performance
- Horse Power/Weight Ratio 0.148
- Wing Loading 25.0lbs/ft2 (122.3kg/m2)
- Wing Area 269.1ft2 (25.0m2)
- Drag Points 3325
Parts
- Number of Parts 73
- Control Surfaces 4
- Performance Cost 280