Search Results - Nettles, A. T. (Alan T.)

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  1. 1

    Simplification of fatigue test requirements for damage tolerance of composite interstage launch vehicle hardware by Nettles, A. T. (Alan T.)

    Published: National Aeronautics and Space Administration, Marshall Space Flight Center, 2010
    Description: 1 online resource (27 pages) : illustrations.
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    Simplification of fatigue test requirements for damage tolerance of composite interstage launch vehicle hardware
  2. 2

    The effects of foam thermal protection system on the damage tolerance characteristics of composite sandwich structures for launch vehicles by Nettles, A. T. (Alan T.)

    Published: National Aeronautics and Space Administration, Marshall Space Flight Center, 2011
    Description: 1 online resource (vii, 23 pages) : illustrations.
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    The effects of foam thermal protection system on the damage tolerance characteristics of composite sandwich structures for launch vehicles
  3. 3

    A comparison of quasi-static indentation to low-velocity impact by Nettles, A. T. (Alan T.)

    Published: National Aeronautics and Space Administration, Marshall Space Flight Center, 2000
    Description: 1 online resource (x, 83 pages) : illustrations.
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    A comparison of quasi-static indentation to low-velocity impact
  4. 4

    A comparison of quasi-static indentation to low-velocity impact by Nettles, A. T. (Alan T.)

    Published: National Aeronautics and Space Administration, Marshall Space Flight Center, 2000
    Description: x, 83 pages : illustrations ; 28 cm.
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    A comparison of quasi-static indentation to low-velocity impact
  5. 5

    Normalization of impact energy by laminate thickness for compression after impact testing by Nettles, A. T. (Alan T.), Hromisin, S. M.

    Published: National Aeronautics and Space Administration, Marshall Space Flight Center, 2013
    Description: 1 online resource (ix, 37 pages) : illustrations (some color).
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    Normalization of impact energy by laminate thickness for compression after impact testing
  6. 6

    The effects of compressive preloads on the compression-after-impact strength of carbon/epoxy by Nettles, A. T. (Alan T.), Lance, D. G.

    Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical, Information Program, 1992
    Description: 1 online resource (iv, 16 pages) : illustrations.
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    The effects of compressive preloads on the compression-after-impact strength of carbon/epoxy
  7. 7

    An examination of the damage tolerance enhancement of carbon/epoxy using an outer lamina of Spectra by Lance, D. G., Nettles, A. T. (Alan T.)

    Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991
    Description: 1 online resource (iv, 27 pages) : illustrations.
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    An examination of the damage tolerance enhancement of carbon/epoxy using an outer lamina of Spectra
  8. 8

    Low velocity instrumented impact testing of four new damage tolerant carbon/epoxy composite systems by Lance, D. G.

    Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; For sale by the National Technical Information Service, 1990
    Description: iv, 34 pages, 1 unnumbered page : illustrations ; 28 cm.
    Other Authors: “…Nettles, A. T. (Alan T.)…”
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    Low velocity instrumented impact testing of four new damage tolerant carbon/epoxy composite systems
  9. 9

    Comparison of open-hole compression strength and compression after impact strength on carbon fiber/epoxy laminates for the Ares I composite interstage by Hodge, A. J.

    Published: National Aeronautics and Space Administration, Marshall Space Flight Center, 2011
    Description: 1 online resource (viii, 23 pages) : illustrations (some color).
    Other Authors: “…Nettles, A. T. (Alan T.)…”
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    Comparison of open-hole compression strength and compression after impact strength on carbon fiber/epoxy laminates for the Ares I composite interstage

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