The DH 108 featured a tailless, swept wing with a single vertical stabilizer, similar to the layout of the wartime German Messerschmitt Me 163 Komet.[1] Despite the Comet design taking on more conventional features, the value of testing the unique configuration to provide basic data for the DH.110[2] spurred de Havilland to continue development of the DH 108.[2] Control was based on the conventional rudder in combination with elevons that were part elevator and ailerons, fitted outboard of the split trailing edge flaps.[5] In later low-speed testing designed to clear the rear fuselage at high angles of attack, the first prototype was fitted with longer Sea Vampire landing gear.[6] The second, high-speed, prototype, TG306, which had a 45° swept wing incorporating automatic leading-edge Handley Page slats and was powered by a de Havilland Goblin 3 turbojet, flew soon afterwards, in June 1946.Modifications to the design included a longer more streamlined nose and a smaller canopy (framed by a strengthened metal fairing) facilitated by lowering the pilot's seat.The subsequent accident investigation centred on a structural failure which occurred as air built up at Mach 0.9, pitching the aircraft into a shock stall that placed tremendous loads on the fuselage and wings.Finally, on 1 May 1950, during low-speed sideslip and stall tests, the first prototype, TG283, was lost in a crash at Hartley Wintney killing the pilot, Sqn Ldr George E.C.