Category:F-8E Crusader

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Vought F-8E Crusader (before 1962: F8U-2NE): J57-P-20A engine, AN/APQ-94 radar in a larger nose cone, dorsal hump between the wings containing electronics for the AGM-12 Bullpup missile, payload increased to 5,000 lb (2,270 kg), Martin-Baker ejection seat, AN/APQ-94 radar replaced AN/APQ-83 radar in earlier F-8D. First flight: 30 June 1961, 286 built.