During 2003 and 2004, the Johnson Space Center's White Sands Testing Facility in Las Cruces, New Mexico conducted hypervelocity impact tests on the space shuttle wing leading edge. Hypervelocity impact tests were conducted to determine if Micro-Meteoroid/Orbital Debris impacts could be reliably detected and located using simple passive ultrasonic methods. The objective of Target RCC16R was to study hypervelocity impacts through the reinforced carbon-carbon (RCC) panels of the Wing Leading Edge. Impact damage was detected using lightweight, low power instrumentation capable of being used in flight.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Hypervelocity Impact (HVI), Volume 7, WLE High Fidelity Specimen RCC16R


    Contributors:
    M. R. Gorman (author) / S. M. Ziola (author)

    Publication date :

    2007


    Size :

    110 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






    Hypervelocity Impact (HVI)

    Gorman, Michael R. / Ziola, Steven M. | NTRS | 2007


    Hypervelocity Impact (HVI)

    Gorman, Michael R. / Ziola, Steven M. | NTRS | 2007


    Hypervelocity Impact Physics

    W. P. Schonberg / A. J. Bean / K. Darzi | NTIS | 1991