The C.23 BN.2 was designed to be a night bomber able to reach
Berlin with a bomb load. The French BN.2 military category indicated a two-seat night bomber but the C.23 had a crew of three. It had much in common with the
Caudron C.22 but was almost 50% larger in span, requiring an extra
bay and more powerful engines. It was a large
five bay biplane, with
fabric covered, constant
chord, unswept wings with angled tips. The upper wing, which carried the
ailerons, had a slightly greater (4%) span and a smaller chord. There was no
stagger, so the sets of parallel
interplane struts were vertical;
flying wires braced each bay. Pairs of V-form engine bearing struts, which supported the two neatly
cowled Salmson 9Z nine cylinder water-cooled
radial engines just above the lower wing, defined the inner two bays. The C.23 had a flat sided
fuselage. There was a gunner's position in the nose, equipped with twin
Lewis guns. A roomy open
cockpit was positioned under the wing
leading edge, with a separate gunner's cockpit behind it under a large, rounded
trailing edge cut-out. This was fitted with another pair of Lewis guns and a further gun firing downwards through a trapdoor in the floor. A low, broad
fin carried a broad
balanced rudder which extended down to the keel. The
tailplane, angular in plan and of very low
aspect ratio, was mounted on top of the fuselage and its
elevators had cut-outs for rudder movement. The bomber had a fixed
tailskid undercarriage, with mainwheels in pairs, their axles mounted on longitudinal bars attached to the wing, under the engines, by N-form
struts. The Caudron C.23 first flew in February 1918, piloted by
Jules Védrines. Higher power engines, the
Salmson 18Z or the
Hispano-Suiza 8Fb, were considered in April 1918 but the Salmson was not yet fully developed and trials with the Hispano led nowhere. ==Operational history==