In March 1929, Flight Lieutenant
Nicholas Comper left the
Royal Air Force and formed the
Comper Aircraft Company with the purpose of building an aircraft that he had designed, which he named the
Comper Swift. A key design goal set by Comper for the Swift was to minimise the presence of
blind spots, a factor that had undermined the prospects of countless aircraft that were otherwise ideal. This principal of prioritising optimal external visibility for the pilot dictated many attributes and characteristics of the aircraft, such as the placement of the
cockpit aft of the high-mounted wing. This in turn necessitated the use of a relatively lightweight engine in order to maintain appropriate weight distribution across the aircraft as there was a considerable amount of vertical surface area placed forward of the
center of gravity. This initial aircraft was powered by a 40 hp (30 kW)
ABC Scorpion piston engine. After successful tests, seven more aircraft were built in 1930, powered by a 50 hp
Salmson A.D.9 radial engine. Trials with
Pobjoy P radial engine for use in air racing resulted in all the subsequent aircraft being powered by the
Pobjoy R. The last three factory-built aircraft (sometimes referred to as the
Gipsy Swift) were fitted with
de Havilland Gipsy engines – two with 120 hp (89 kW) Gipsy Major III, and one with a 130 hp (97 kW) Gipsy Major. ==Design==