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Vought Model 1600

Military Aircraft

The Vought Model 1600 was a carrier-based fighter proposal that Vought and General Dynamics put to the United States Navy in the mid 1970s for its Navy Air Combat Fighter program. It was a navalized derivative of the General Dynamics F-16 Fighting Falcon, built on the Block 10 airframe with structural strengthening, an arrestor hook and a more robust undercarriage for carrier launch and recovery. General Dynamics had no carrier aircraft experience and so teamed up with Vought, whose F-8 Crusader and A-7 Corsair II had served the Navy well. Vought drew up three concepts, the Model 1600 with a Pratt & Whitney F401 turbofan, the Model 1601 with an improved F100 and the Model 1602 with a General Electric F101. The Navy preferred a twin-engine aircraft and on 2 May 1975 chose the Northrop and McDonnell Douglas design that became the F/A-18 Hornet, so the Model 1600 was never built.

Facts
Engine Class
Turbofan 1
Status
Design only (never built) 1
Maximum Mass (kg)
14,166 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Vought Model 1600 (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Vought Model 1600 (Wikipedia)Development
Quote, Development
General Dynamics teamed up with Vought (LTV Aerospace)

Originated In

Also in Geography Atlas: where this subject originated.

Source Vought Model 1600 (Wikipedia)Lead, country of origin
Quote, Lead, country of origin
was a fighter aircraft proposal for the United States Navy's Navy Air Combat Fighter (NACF) program
Sources
1. Vought Model 1600 (Wikipedia)
  • Lead
    The Vought/General Dynamics Model 1600 series was a fighter aircraft proposal for the United States Navy's Navy Air Combat Fighter (NACF) program.
  • Variants, Model 1600
    It was powered by the Pratt & Whitney F401 (JTF22A-26C) afterburning turbofan.
  • Lead, outcome
    The Model 1600 was a carrier-based derivative of the General Dynamics F-16 Fighting Falcon, but lost to the Northrop/McDonnell Douglas F/A-18 Hornet.
  • Specifications
    Max takeoff weight: 31,231 lb (14,166 kg)
  • Development
    General Dynamics teamed up with Vought (LTV Aerospace)
  • Lead, country of origin
    was a fighter aircraft proposal for the United States Navy's Navy Air Combat Fighter (NACF) program
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