Problems encountered in providing h-p hot-gas source to turbine of aircraft engine starter, methods of solving these problems, and design procedures followed in arriving at solid-propellant cartridge which functioned in all environments encountered in both storage and operation; development techniques and results of experimental investigations are presented.


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    Title :

    Development of cartridges for aircraft engine cartridge starters


    Additional title:

    ASME -- Paper


    Contributors:

    Conference:

    ASME Meeting GT-21 ; 1967 Starting



    Publication date :

    1967


    Size :

    11 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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