In configuration, the Camel featured equal-span, staggered bi-plane wings (the lower with some dihedral) featuring only a single pair of parallel support struts. Construction consisted of an underlying structure made up mostly of wood covered in fabric with some light alloy skinning over the forward fuselage near the engine. The pilot sat to the rear and underneath the upper wing element. In fact, all major systems were purposefully positioned in the front 7 feet of the fuselage, this including the main landing gears, engine, wings, armament and pilot. Armament consisted of 2 x 7.7mm Vickers-type machine guns firing through the propeller via an interrupter gear (i.e. synchronized). The designation of "Camel" came from the hump created by the fairing over the breeches of these gun installations. Power of the F.1 model was derived from a Clerget 9B 9-cylinder rotary engine of 130 horsepower providing speeds of 115 miles per hour, a ceiling of over 20,000 feet and a range of 485 kilometers.