Supersonic air transports will require electrical systems capable of withstanding temperatures estimated at 600 F. The suitability of various materials is discussed with respect to use as conductor and as insulation, and components including resistors, transformers, capacitors, rectifiers, and tubes. The Air Force Hotelec program is reviewed with the significant test results. Areas of required additional development work are listed.


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    Title :

    High Temperature Electrical System Development Applicable to Supersonic Transports


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    Pre-1964 SAE Technical Papers ; 1906



    Publication date :

    1962-01-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





    Airworthiness codes as applicable to supersonic transports

    Fenner, R.J. | Engineering Index Backfile | 1966



    Supersonic Transports

    Online Contents | 1994


    Materials for supersonic transports

    RARING, R. | AIAA | 1964