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  • The effects of embedded internal delaminations on composite laminate compression strength [microform] : an experimental review / by Alan T. Nettles.

    • Text
    • [Marshall Space Flight Center, Ala.] : National Aeronautics and Space Administration, George C. Marshall Space Flight Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • The effects of compressive preloads on the compression-after-impact strength of carbon/epoxy [microform] / Alan T. Nettles.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Low temperature mechanical testing of carbon-fiber/epoxy-resin composite materials [microform] / Alan T. Nettles and Emily J. Biss.

    • Text
    • Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Scaling effects in carbon/epoxy laminates under transverse quasi-staic loading [microform] / Alan T. Nettles, Michael J. Douglas, Eric E. Estes.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999

  • A damage resistance comparison between candidate polymer matrix composite feedline materials [microform] / A.T. Nettles.

    • Text
    • Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center ; Hanover, MD : Available from NASA Center for AeroSpace Information, [2000]
    • 2000
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS22780

  • Permeability testing of impacted composite laminates for use on reusable launch vehicles [microform] / A.T. Nettles.

    • Text
    • Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center ; Hanover, MD : Available from NASA Center for AeroSpace Information, [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS23038

  • Polymer matrix composite lines and ducts [microform] / A.T. Nettles.

    • Text
    • Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center ; Hanover, MD : Available from NASA Center for AeroSpace Information, [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS26613

  • An examination of impact damage in glass/phenolic and aluminum honeycomb core composite panels [microform] / A.T. Nettles, D.G. Lance, and A.J. Hodge.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, VA : For sale by the National Technical Information Service], 1990.
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS65683

  • Cross-sectional examination of the damage zone in impacted specimens of carbon/epoxy and carbon/peek composites [microform] / by A.T. Nettles and N.J. Magold.

    • Text
    • [Marshall Space Flight Center, Ala.] : National Aeronautics and Space Administration, George C. Marshall Space Flight Center ; [Springfield, VA : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67327

  • Instrumented impact and residual tensile strength testing of eight-ply carbon/epoxy specimens [microform] / A.T. Nettles.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, VA : For sale by the National Technical Information Service], 1990.
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS68606

  • A damage tolerance comparison of composite hat-stiffened and honeycomb sandwich structure for launch vehicle interstage applications / A.T. Nettles.

    • Text
    • Huntsville, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24323

  • A comparison of quasi-static indentation to low-velocity impact / A. T. Nettles, M. J. Douglas.

    • Text
    • [Marshall Space Flight Center, AL] : National Aeronautics and Space Administration, Marshall Space Flight Center, [2000]
    • 2000
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo33154

  • A comparison of quasi-static indentation to low-velocity impact [microform] / A. T. Nettles, M. J. Douglas.

    • Text
    • [Marshall Space Flight Center, AL] : National Aeronautics and Space Administration, Marshall Space Flight Center, [2000]
    • 2000

  • The impact response of carbon/epoxy laminates / A.T. Nettles and A.J. Hodge.

    • Text
    • Marshall Space Flight Center, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, November 1997.
    • 1997-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo79004

  • Permeability testing of impacted composite laminates for use on reusable launch vehicles / A.T. Nettles.

    • Text
    • MSFC, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, February 2001.
    • 2001-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS23038

  • The effect of impact damage next to holes on the bearing strength of carbon fiber laminates / A.T. Nettles.

    • Text
    • Huntsville, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, December 2019.
    • 2019-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo130586

  • Normalization of impact energy by laminate thickness for compression after impact testing / A.T. Nettles and S.M. Hromisin.

    • Text
    • Huntsville, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, 2013.
    • 2013
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37983

  • A quantitative damage tolerance comparison of high strength and high modulus carbon fiber sandwich structure / A.T. Nettles, W.E. Guin, and C.C. Wolfe.

    • Text
    • Huntsville, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, January 2022.
    • 2022-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo174309

  • A damage resistance comparison of wet-wound IM7 and T1100 carbon fiber/epoxy cylinders / A.T. Nettles and A.M. Clark.

    • Text
    • Huntsville, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, April 2022.
    • 2022-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo177589

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