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Douglas F6D Missileer

Military Aircraft

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
Jet 1
Status
Cancelled 1
Maximum Mass (kg)
27,216 1
Comparison
Body Style
Aircraft (no road body style) 1
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Exemplifies

Aviation, Modes
Source Douglas F6D Missileer (Wikipedia)

Of Make

Source Douglas F6D Missileer (Wikipedia)
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Manufactured By

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Source Douglas F6D Missileer (Wikipedia)Lead, manufacturer
Quote, 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, manufacturer
Quote, 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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