Developed as an all-weather version of the Douglas F4D, the F5D Skylancer first flew on 21 April 1956. It used a more powerful engine (Pratt & Whitney J57 – the first 45kN thrust class turbojet engine). Compare to the F4d, the wing was thinner, but more reinforced, the fuselage was area-ruled, reducing transonic drag and was 2.4m longer.
Originally nine test aircraft were ordered, with a 51 production run to follow, although only four of the test aircraft were built. During testing, the US Navy decided that the Skylancer was too similar to the Vought F8U Crusader that was already in service and canceled the contract.
The F5Ds continued as test aircraft, being passed on to NASA in the early 1960s, two were grounded and used for spare parts. One was used as a testbed for the American supersonic transport program, fitted with an ogival wing platform (the type eventually used on Concorde). Data from the program was shared with the European designers.
Both of the aircraft used by NASA were used to support the Dyna-Soar project. One was retired in 1968 followed by the second in 1970.