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  2. Fairchild Republic A-10 Thunderbolt II - Wikipedia

    en.wikipedia.org/wiki/Fairchild_Republic_A-10...

    In 2014, as part of plans to retire the A-10, the USAF considered halting the wing replacement program to save an additional $500 million; [42] [43] however, by May 2015 the re-winging program was too advanced to be financially efficient to cancel. [44] Boeing stated in February 2016 that the A-10 could operate to 2040 with the new TUSK wings. [39]

  3. Grumman A-6 Intruder - Wikipedia

    en.wikipedia.org/wiki/Grumman_A-6_Intruder

    Pre-production aircraft, eight built with the first four with rotating jet exhaust pipes, redesignated YA-6A in 1962. [40] A2F-1 First production variant with fixed tailpipe, 484 built, redesignated A-6A in 1962. [40] YA2F-1H Prototype electronic warfare variant, one modified from A2F-1, redesignated YEA-6A in 1962. [40] A2F-1H

  4. GAU-8 Avenger - Wikipedia

    en.wikipedia.org/wiki/GAU-8_Avenger

    The General Electric GAU-8/A Avenger is a 30 mm hydraulically driven seven-barrel Gatling-style autocannon that is primarily mounted in the United States Air Force's Fairchild Republic A-10 Thunderbolt II.

  5. Propelling nozzle - Wikipedia

    en.wikipedia.org/wiki/Propelling_nozzle

    A propelling nozzle is a nozzle that converts the internal energy of a working gas into propulsive force; it is the nozzle, which forms a jet, that separates a gas turbine, or gas generator, from a jet engine. Propelling nozzles accelerate the available gas to subsonic, transonic, or supersonic velocities depending on the power setting of the ...

  6. Northrop YF-23 - Wikipedia

    en.wikipedia.org/wiki/Northrop_YF-23

    The aircraft had single-expansion ramp nozzles (SERN) and, unlike the YF-22, did not employ thrust vectoring. [29] As on the B-2, the exhaust from the YF-23's engines flowed through troughs in the aft deck to shield the engines from infrared homing (IR) missile detection from below.

  7. Exhaust mixer - Wikipedia

    en.wikipedia.org/wiki/Exhaust_mixer

    The exhaust thrust from a jet engine is equal to exhaust mass flow times exhaust velocity, i.e., Thrust = ṁv, while the energy to make that thrust is given by Energy = 1/2mv 2. A mixer helps reduce the fastest exhaust velocities from the core of the engine, while making the average exhaust velocity faster, producing more thrust with the same ...

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