Materials evaluation, design and fabrication work, and low pressure testing to develop high temperature hydraulic system actuator seals for use in advanced supersonic aircraft


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    High temperature hydraulic system actuator seals for use in advanced supersonic aircraft Semiannual report


    Contributors:
    Lee, J. (author)

    Publication date :

    1966-10-14


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English