The Douglas F5D Skylancer is a development of the F4D Skyrayjet fighter for the United States Navy. Starting out as the F4D-2N, an all-weather version of the Skyray, the design was soon modified to take full advantage of the extra thrust of the Pratt & Whitney J57 eventually fitted to the Skyray instead of the Westinghouse J40 originally planned.
Design and development
Soon the design became too different from the Skyray to be considered just a variation of it, and the aircraft was assigned a new designation as the F5D Skylancer. Almost every part of the airframe was modified, though the basic form remained the same as did the wing shape, though it became much thinner. The wing skinning was reinforced, correcting a problem found in the F4D. The fuselage was 8 ft (2.4 m) longer and area ruled to reduce transonic drag, being thinner in the region of the wing roots. Everything was shaped to reduce drag and increase stability at high speed.
Although the four 20 mm (.79 in) cannon in the wing roots were retained, primary armament was to be missiles or rockets; four AIM-9 Sidewinders or two AIM-7 Sparrows, and/or a battery of spin-stabilized unguided 2 in (51 mm) rockets.
Nine test airframes were ordered, with a 51-aircraft production order to follow. Production aircraft were to be powered by the more powerful J57-P-14 engine, while there was a rejected proposal to use the even more powerful General Electric J79 and variable-geometry inlets in a Mach 2 version.[1]
Operational history
The first flight was made by F5D-1 (Bu. No. 139208)[2] on 21 April 1956 and was supersonic; the aircraft proved easy to handle and performed well. After four aircraft had been constructed, however, the Navy cancelled its order. The stated reason was that the aircraft was too similar to the already-ordered Vought F8U Crusader, but it is believed by some historians that politics played as big a part; Douglas was already building a very large proportion of the Navy's planes, and giving them the F5D contract would have made it even closer to monopoly.[3] The project test pilot was Lt. Cmdr Alan B. Shepard Jr. whose report stated that it was not needed by the Navy. One F5D crashed during testing by the Navy.[4]
The four aircraft continued to fly in various military test programs. Two were grounded in 1961 (likely 139209 and 142349 which had been designated for spare parts in 1958[5]), but the other two: F5D-1 (Bu. No. 139208) NASA 212,[6] later becoming NASA 708 and F5D-1 (Bu. No. 142350) NASA 213, later becoming NASA 802 continued to fly. Transferred to NASA in the early 1960s, NASA 212 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),[7] as well as being used as a vision field test platform for the X-20 Dyna-Soar.[8] This aircraft was retired in 1968. NASA 802 was used for simulation of abort procedures for the X-20, because it had a very similar shape and handling characteristics. Following the DynaSoar cancellation, it was used as a chase plane and for various other programs until it was retired in 1970.[9]
Data from Naval Fighters#35 : Douglas F5D-1 Skylancer,[15] McDonnell Douglas aircraft since 1920 : Volume I,[16] The American Fighter[17]
General characteristics
Crew: 1
Length: 53 ft 9.75 in (16.4021 m)
Wingspan: 33 ft 6 in (10.21 m) wings spread
Width: 27 ft 6 in (8.38 m) wings folded
Height: 14 ft 10 in (4.52 m)
Wing area: 557 sq ft (51.7 m2)
Empty weight: 17,444 lb (7,912 kg)
Empty equipped: 18,147 lb (8,231 kg)
Maximum landing weight: 21,320 lb (9,670 kg)
Gross weight: 27,739 lb (12,582 kg) full internal fuel + 72x 2 in (51 mm) rockets
28,739 lb (13,036 kg) with full internal fuel + 72x 2 in (51 mm) rockets + 2x AIM-7 Sparrow II AAMs
Max takeoff weight: 31,204 lb (14,154 kg) with full internal fuel + 72x 2 in (51 mm) rockets + 2x AIM-7 Sparrow II AAMs + 2x 150 US gal (120 imp gal; 570 L) drop-tanks
Fuel capacity: 1,353 US gal (1,127 imp gal; 5,120 L) JP-5 in two fuselage tanks and four wing tanks; Usable fuel 1,333 US gal (1,110 imp gal; 5,050 L)
Angelucci, Enzo. The American Fighter. Sparkford, Somerset, UK: Haynes Publishing Group, 1987. ISBN0-85429-635-2.
Frankel, Mark. Killer Rays: The Story of the Douglas F4D Skyray and F5D Skylancer. North Branch, Minnesota: Specialty Press, 2010. ISBN978-1-58007-155-0.
Ginter, Steve. Douglas F5D-1 Skylancer (Naval Fighters No. 35). Simi Valley, California: Ginter Books, 1996. ISBN0-942612-35-3.
Gunston, Bill. Fighters of the Fifties. Cambridge, UK: Patrick Stephens Limited, 1981. ISBN0-85059-463-4.
Winchester, Jim, ed. "Douglas F4D Skyray." Military Aircraft of the Cold War (The Aviation Factfile). London: Grange Books plc, 2006. ISBN1-84013-929-3.
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