Design
The F6D-1 would have weighed approximately 50,000 lb (22,650 kg). It would have been powered by two Pratt & Whitney TF30-P2 non-afterburning turbofan engines which were more fuel efficient than the turbojets common at the time. It would have had subsonic performance, but a loiter time of six hours on station 150 nmi (280 km) from its carrier. Of conventional design with straight wings, and the engines in pods at the root, it looked like a larger version of the company's earlier F3D Skyknight. The Missileer's radar was to be the Westinghouse AN/APQ-81 pulse Doppler set, with a range of 120 nmi (220 km) and "track while scan" capability. It was to be able to engage up to six targets simultaneously with Bendix AAM-N-10 Eagle air-to-air missiles, with a range of 100 nmi (185 km). The Eagle was to have a choice of conventional or nuclear warhead.
Read more about this topic: Douglas F6D Missileer
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