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In December 1944 Hawker refined the proposed design substantially. The jet exhaust was moved from beneath the tail and re-designed as two short split-lateral bifurcated exhausts (which gained the name "trouser legs"), embedded in the trailing edge of the wing root, which needed a corresponding thickening of the wing root; the air intakes were moved to the wing root leading edge, similar to the contemporary de Havilland Vampire. The shorter unusual bifurcated jet pipe reduced pressure losses in the jet pipe and had the additional advantage of freeing up space in the rear fuselage for fuel tanks, which gave the aircraft a longer range than many other early jets. The absence of wing fuel tanks also meant a thinner wing could be adopted without the penalty of reduced range; to ease manufacture, the elliptical wingform of the Fury was discarded in favour of a straight tapered wing design. The fuselage fuel tanks, being fore and aft of the engine, also provided for a stable centre of gravity during flight. The tail plane was raised to clear the jet exhausts. The Sea Hawk also featured a nose wheel undercarriage arrangement, the first for a Hawker-built aircraft. The aircraft was built to accommodate four 20mm Hispano-Suiza Mk. V cannon.
Ceiling
Combat RANGE
Aircraft Speed
Max Crew
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The first prototype flew on 2 September, 1947; the project was announced to the public a month later, disguised for some forgotten reason as a purely company-financed effort. This pretense was dropped when the second prototype flew a year later, on 3 September, 1948: it had folding wings, a stinger-type arresting hook, and was fully armed. This second prototype was used in carrier trials that indicated a need for a slightly longer wingspan and arresting hook
Also in 1956, 22 Sea Hawks were ordered by the Dutch to operate with the Naval Air Service (Marine Luchtvaartdienst - MLD)
Also in 1956, 22 Sea Hawks were ordered by the Dutch to operate with the Naval Air Service (Marine Luchtvaartdienst - MLD)