The effect of various lubricants and other compounds on fastener torque-tension relationships is evaluated. Testing was performed using a unique test apparatus developed by Posey at the NASA Goddard Space Flight Center. A description of the test methodology, including associated data collection and analysis will be presented. Test results for 300 series CRES and A286 heat resistant fasteners, torqued into various types of inserts will be presented. The primary objective of this testing was to obtain torque-tension data for use on NASA flight projects.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Torque Tension Testing of Fasteners used for NASA Flight Hardware Applications


    Contributors:
    E. Hemminger (author) / A. Posey (author) / M. Dube (author)

    Publication date :

    2014


    Size :

    14 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Torque Tension Testing of Fasteners used for NASA Flight Hardware Applications

    Hemminger, Edgar G. / Posey, Alan J. / Dube, Michael J. | NTRS | 2014


    Torque Tension Testing of Fasteners used for NASA Flight Hardware Applications

    E. G. Hemminger / A. J. Posey / M. J. Dube | NTIS | 2014


    Torque Tension Testing of Fasteners used for NASA Flight Hardware Applications

    Hemminger, Ed / Posey, Alan / Dube, Michael | NTRS | 2014