F5D Skylancer
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Douglas F5D Skylancer prototype in use by NASA for Dyna-Soar abort training. |
The
Douglas F5D Skylancer was a development of the
F4D Skyray 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.
Soon the design became too different to 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 feet (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 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 were plans to use the even more powerful
General Electric J79.
The first flight was on
April 21,
1956 and was supersonic; the aircraft proved itself easy to handle and perform excellently. However, after four aircraft had been constructed, the Navy cancelled its order. The stated reason was that the aircraft was too similar to the already-ordered
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.
The four aircraft continued to fly in various military test programs. Two were grounded in
1961, but the other two continued to fly; transferred to
NACA (soon to become
NASA) in the early
1960s, 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). This aircraft was retired in
1968. The other (pictured) was used for simulation of abort procedures for the
X-20 DynaSoar, 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. This last plane still exists at the
Armstrong Air and Space Museum at
Wapakoneta, Ohio, since
Neil Armstrong flew the plane during the DynaSoar program.
{{aircraft specification|
plane or copter?=plane | >crew=1 | length main=53 ft 9¾ in | length alt=16.40 m | span main=33 ft 6 in | span alt=10.21 m | height main=14 ft 10 in | height alt=4.52 m | area main=557 ft² | area alt=51.7 m² | empty weight main=17,444 lb | empty weight alt=7,912 kg | loaded weight main=24,445 lb | loaded weight alt=11,088 kg | max takeoff weight main=28,072 lb | max takeoff weight alt=12,733 kg | engine (jet)=Pratt & Whitney J57-P-8 | type of jet=turbojet | number of jets=1 | thrust main=10,200 lbf dry; 16,000 lbf afterburner | thrust alt=45 kN / 71 kN | max speed main=990 mph | max speed alt=1,590 km/h | range main=1,335 mi | range alt=2,148 km | ceiling main=57,500 ft | ceiling alt=17,500 m | climb rate main=20,730 ft/min | climb rate alt=105.3 m/s | loading main=lb/ft² | loading alt=kg/m² | thrust/weight=0.65 | avionics= * X-24A radar | armament= *4x 20 mm cannons *4x AIM-9 Sidewinder or 2x AIM-7 Sparrow missiles *72x 2 in (51 mm) rockets{{aircontent | sequence=XFD - XF2D - F3D - F4D - F5D - F6D|related= *F4D Skyray|similar aircraft= *F8U Crusader|lists=|see also=
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