The vertical tail surfaces were mounted at the ends of twin booms, with the V-tail plane in between the fins and supported at its center by a dorsal fin on the aft end of the fuselage. Separate air inlets were provided for the two engines; in the wing roots for the lower engine and on the side of the rear fuselage for the upper engine. The landing gear was a retractable tricycle. The aircraft was first flown on July 24, 1954.
Span: 17 ft 2 in (5.25 m)
Length: 19 ft 7 in (5.97 m)
Height: 5 ft 9 in (1.77 m)
Loaded weight: 2,420 lb (1,100 kg)
Max speed: 466 mph (750 kmh)
Min speed: 118 mph (190 kmh)
Duration: 75 min