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  • Test plan, task 5, subtask 5.2, early on-orbit TPS debris impact tests [microform] / H.S. Greenberg, principal investigator.

    • Text
    • [Downey, Calif.] : Rockwell Aerospace, Space Systems Division ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Influence of temperature and impact velocity on the coefficient of restitution [microform] / Kevin C. Radil.

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

  • Response of composite materials to low velocity impact [microform] / K. Srinivasan, W.C. Jackson and J.A. Hinkley.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [St. Louis, Mo.] : US Army Aviation Systems Command, Aviation R&T Activity ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • Determination of the relative resistance to ignition of selected turbopump materials in high-pressure, high-temperature, oxygen environments [microform] : test report.

    • Text
    • Las Cruces, N.M. : Lyndon B. Johnson Space Center, White Sands Test Facility : [Washington, D.C. : National Aeronautics and Space Administration, ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Milestone 4 [microform] : test plan for reusable hydrogen composite tank system (RHCTS) : task 3, composite tank materials / H.S. Greenberg, principal investigator.

    • Text
    • [Downey, Calif.] : Rockwell Aerospace, Space Systems Division ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Optimization techniques applied to passive measures for in-orbit spacecraft survivability [microform] / prepared by Robert A. Mog, Michael J. Helba, Janeil B. Hill.

    • Text
    • Huntsville, AL. : SAIC ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • Impact damage resistance and residual property assessment of [0/+/-45/90]s SCS-6/Timetal 21S [microform] / Jennifer L. Miller, Marc A. Portanova, W. Steven Johnson.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Design and testing of an energy-absorbing crewseat for the F/FB-111 aircraft [microform] / S. Joseph Shane.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : National Technical Information Service, distributor], 1985-
    • 1985-present

  • Composite processing development to improve interlaminar strength using ply interface particles [microform] : (Center Director's discretionary fund final report, no. 93-13) / A.T. Nettles.

    • Text
    • MSFC, Ala. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Duplication and analysis of meteoroid damage on LDEF and advanced spacecraft materials [microform] : final report for NASA research grant NAG-1-1329, 1 January 1993 - 31 December 1994 / David C. Hill & M. Frank Rose, project investigators.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Annual performance report [microform] : planetary and primitive object strength measurement and sampling apparatus : NASA/Washington grant NAGW-2439, for the period 2/1/95-1/31/96 (year two) / principal investigator, Thomas J. Ahrens.

    • Text
    • Pasadena, CA : California Institute of Technology, Seismological Laboratory ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Penetration experiments in aluminum 1100 targets using soda-lime glass projectiles [microform] / Friedrich Hörz ... [et al.].

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • NSTAR ion thruster plume impacts assessments [microform] / Roger M. Myers ... [et al.].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • The effects of tensile preloads on the impact response of carbon/epoxy laminates [microform] / Alan Nettles, Vince Daniel, Caleb Branscomb.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Evaluation of the impact response of textile composites [microform] / M.A. Portanova.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • 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

  • Elevated temperature ballistic impact testing of PBO and Kevlar fabrics for application in supersonic jet engine fan containment systems [microform] / J. Michael Pereira, Gary D. Roberts, and Duane M. Revilock.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Damage characteristics and residual strength of composite sandwaich panels impacted with and without compression loading [microform] / : presented at the 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, session no. 15-damage tolerance : Long Beach, California, April 20-23, 1998 / David M. McGowan and Damodar R. Ambur.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

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

    • Text
    • [Huntsville, Ala.] : National Aeronautics and Space Administration, Marshall Space Flight Center ; Springfield, VA : National Technical Information Service, distributor, [1997]
    • 1997

  • SEDS tether M/OD damage analyses [microform] / K.B. Hayashida, J.H. Robinson, and S.A. Hill.

    • Text
    • [Marshall Space Flight Center, Ala.] : National Aeronautics and Space Administration, Marshall Space Flight Center ; Springfield, VA : National Technical Information Service, distributor, [1997]
    • 1997

  • 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

  • Crashworthy evaluation of a 1/5-scale model composite fuselage concept [microform] / Karen E. Jackson and Edwin L. Fasanella.

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

  • 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

  • Impact testing of composites for aircraft engine fan cases [microform] / Gary D. Roberts ... [et al.].

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS26848

  • 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

  • Dynamic finite element predictions for Mars sample return cellular impact test #4 [microform] / Edwin L. Fasanella, Marcus D. Billings.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover MD : Available from NASA Center for AeroSpace Information (CASI), [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS27476

  • Full-scale transport controlled impact demonstration [microform] : proceedings of a workshop sponsored by NASA Langley Research Center, Hampton, Virginia, and the FAA Technical Center, Atlantic City, New Jersey, and held in Hampton, Virginia, April 10, 1985 / Robert J. Hayduk, compiler.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986.
    • 1986

  • Design and testing of an energy-absorbing crewseat for the F/FB-111 aircraft [microform] : volume II, data from seat testing / S. Joseph Shane.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985.
    • 1985

  • Modeling of high-strain-rate deformation, fracture, and impact behavior of advanced gas turbine engine materials at low and elevated temperatures [microform] / Mostafa Shazly, David Nathenson, and Vikas Prakash.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information ; Springfield, VA : National Technical Information Service [distributor, 2003]
    • 2003
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS55231

  • Hypervelocity impact testing of nickel hydrogen battery cells [microform] / David T. Frate and Henry K. Nahra.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, [Lewis Research Center ; Springfield, Va. : For sale by the National Technical Information Service, 1996]
    • 1996
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60618

  • 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

  • SRB/FWC water impact [microform] : flexible body loads test / prepared by Bolt Beranek and Newman Inc. ; prepared for George C. Marshall Space Flight Center.

    • Text
    • Marshall Space Flight Center, AL : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1984]
    • 1984

  • Composite transport wing technology development [microform] / Ram C. Madan.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1988]
    • 1988
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS89432

  • Ballistic impact testing of aluminum 2024 and titanium 6A1-4V for material model development / J. Michael Pereira ... [and others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo30975

  • 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

  • Elemental water impact test : phase 1 20-inch hemisphere / Gregory J. Vassilakos.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, January 2015.
    • 2015-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo57067

  • Dynamic open-rotor composite shield impact test report / Silvia Seng [and six others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, November 2015.
    • 2015-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo64633

  • Impact and penetration of thin aluminum 2024 flat panels at oblique angles of incidence / Charles R. Ruggeri [and four others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, April 2015.
    • 2015-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65850

  • Experimental and numerical analysis of triaxially braided composites utilizing a modified subcell modeling approach / Christopher Cater [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, June 2015.
    • 2015-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo66954

  • Crash tests of three Cessna 172 Aircraft at NASA Langley Research Center's landing and impact research facility / Justin D. Littell.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, November 2015.
    • 2015-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo67263

  • Elevated temperature ballistic impact testing of PBO and Kevlar fabrics for application in supersonic jet engine fan containment systems / J. Michael Pereira, Gary D. Roberts, and Duane M. Revilock.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, November 1997.
    • 1997-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo73197

  • 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

  • Hypervelocity impact testing of nickel hydrogen battery cells / David T. Frate and Henry K. Nahra.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, September 1996.
    • 1996-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS60618

  • Simulating the impact response of three full-scale crash tests of Cessna 172 aircraft / Karen E. Jackson [and four others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, July 2017.
    • 2017-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo84057

  • 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

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

    https://purl.fdlp.gov/GPO/LPS60878

  • Impact testing of aluminum 2024 and titanium 6A1-4V for material model development / J. Michael Pereira [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2013]
    • 2013
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo40546

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