With availability of power plants incorporating turbosuperchargers with sufficient capacity to super charge engine for high altitude operation, and enough capacity to bleed off sufficient flow and pressure for cabin pressurization, feasibility of pressurized light, single and twin engine aircraft is possible; three different approaches to pressurized light aircraft are discussed, divided into least expensive, medium price, and most expensive approach; tabulation of altitude-pressure-temperature; recommendations and suggestions are also included.


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    Title :

    Pressurization, light aircraft -- Values and controls


    Additional title:

    SAE -- Conference -- Proc


    Contributors:

    Conference:

    Society of Automotive Engineers Conference on Buiness Aircraft ; 1965


    Published in:

    Publication date :

    1965


    Size :

    5 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English







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