The Douglas F6D Missileer was a proposed carrier-based fleet defense fighter designed by the Douglas Aircraft Company in response to a 1959 United States Navy requirement. It was meant to loiter for long periods at a relatively long distance from the Navy carriers and engage hostile aircraft 100 miles away with its powerful radar and long-range missiles; because the enemy would be fired on long before reaching visual range, it had little dogfighting capability and was strictly subsonic. When doubts were raised about its ability to defend itself after firing its missiles, the value of the project was questioned, and the F6D was cancelled in December 1961. Its lasting contribution was its engines, radar and missiles, and the TF30 turbofan with afterburner was used on both the F-111 and the F-14.
Facts
Engine Class Maximum Mass (kg) Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Douglas F6D Missileer (Wikipedia)
Of Make
Source Douglas F6D Missileer (Wikipedia)
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Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Douglas F6D Missileer (Wikipedia)Lead, manufacturerQuote, Lead, manufacturer
designed by Douglas Aircraft Company in response to a 1959 United States Navy requirement
Originated In
Also in Geography Atlas: where this subject originated.
Source Douglas F6D Missileer (Wikipedia)Lead, manufacturerQuote, Lead, manufacturer
designed by Douglas Aircraft Company in response to a 1959 United States Navy requirement
Sources
1. Douglas F6D Missileer (Wikipedia)
Lead
proposed carrier-based fleet defense fighter
Specifications
Pratt & Whitney TF30-P-2 turbofans
Development
led to the cancellation of the F6D in December 1961
Specifications, maximum mass
Max takeoff weight: 60,000 lb (27,216 kg)
Lead, manufacturer
designed by Douglas Aircraft Company in response to a 1959 United States Navy requirement
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