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    F-4 Functional Modernization

    Source: Journal of Engineering for Gas Turbines and Power:;1985:;volume( 107 ):;issue: 004::page 815
    Author:
    W. D. Poulin
    DOI: 10.1115/1.3239816
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Evolving aircraft and engine technologies, as well as advancements in avionics, have resulted in a new generation of fighter aircraft. In order for an air force to remain survivable in such an environment it must face the necessity of either acquiring new aircraft or upgrading its fleet. Today, acquisition of new aircraft may not be an economically or politically viable solution. The newest aircraft, those with a thrust-to-weight ratio exceeding 1 to 1, generally exceed $ 20 million, exclusive of support costs. Politically, sale of such state-of-the-art aircraft to friendly countries may not be possible given the current FX aircraft export policy, and the fiscal posture of the country. However, there is an alternative to new aircraft acquisition, and that is functional modernization: the modernization of potentially viable systems through the implementation of new and available technologies. The Boeing Military Airplane Company and Pratt & Whitney have teamed in the newest aircraft functional modernization proposal, the F-4 Super Phantom. The full modernization package includes a new centerline conformal fuel tank, new digital avionics, and re-engining with new PW1120 engines. This paper examines the initial feasibility study conducted by Pratt & Whitney and Boeing to determine the feasibility of a functionally modernized F-4.
    keyword(s): Weight (Mass) , Engines , Thrust , Aircraft , Fuel storage , Military aircraft , Phantoms , Sales , Air Force AND Avionics ,
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      F-4 Functional Modernization

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    https://yetl.yabesh.ir/yetl1/handle/yetl/99731
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorW. D. Poulin
    date accessioned2017-05-08T23:20:02Z
    date available2017-05-08T23:20:02Z
    date copyrightOctober, 1985
    date issued1985
    identifier issn1528-8919
    identifier otherJETPEZ-26626#815_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/99731
    description abstractEvolving aircraft and engine technologies, as well as advancements in avionics, have resulted in a new generation of fighter aircraft. In order for an air force to remain survivable in such an environment it must face the necessity of either acquiring new aircraft or upgrading its fleet. Today, acquisition of new aircraft may not be an economically or politically viable solution. The newest aircraft, those with a thrust-to-weight ratio exceeding 1 to 1, generally exceed $ 20 million, exclusive of support costs. Politically, sale of such state-of-the-art aircraft to friendly countries may not be possible given the current FX aircraft export policy, and the fiscal posture of the country. However, there is an alternative to new aircraft acquisition, and that is functional modernization: the modernization of potentially viable systems through the implementation of new and available technologies. The Boeing Military Airplane Company and Pratt & Whitney have teamed in the newest aircraft functional modernization proposal, the F-4 Super Phantom. The full modernization package includes a new centerline conformal fuel tank, new digital avionics, and re-engining with new PW1120 engines. This paper examines the initial feasibility study conducted by Pratt & Whitney and Boeing to determine the feasibility of a functionally modernized F-4.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleF-4 Functional Modernization
    typeJournal Paper
    journal volume107
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3239816
    journal fristpage815
    journal lastpage820
    identifier eissn0742-4795
    keywordsWeight (Mass)
    keywordsEngines
    keywordsThrust
    keywordsAircraft
    keywordsFuel storage
    keywordsMilitary aircraft
    keywordsPhantoms
    keywordsSales
    keywordsAir Force AND Avionics
    treeJournal of Engineering for Gas Turbines and Power:;1985:;volume( 107 ):;issue: 004
    contenttypeFulltext
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