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A brief overview of the effects of impact damage to rocket motor cases / / A.T. Nettles
A brief overview of the effects of impact damage to rocket motor cases / / A.T. Nettles
Autore Nettles A. T (Alan T.)
Pubbl/distr/stampa Huntsville, AL : , : George C. Marshall Space Flight Center, , September 2020
Descrizione fisica 1 online resource (various pagings) : color illustrations
Collana NASA/TM
Soggetto topico Impact damage
Launch vehicles
Burst strength
Rocket engine cases
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910713934903321
Nettles A. T (Alan T.)  
Huntsville, AL : , : George C. Marshall Space Flight Center, , September 2020
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
A comparison of quasi-static indentation to low-velocity impact [[electronic resource] /] / A. T. Nettles, M. J. Douglas
A comparison of quasi-static indentation to low-velocity impact [[electronic resource] /] / A. T. Nettles, M. J. Douglas
Autore Nettles A. T (Alan T.)
Pubbl/distr/stampa [Marshall Space Flight Center, AL] : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , [2000]
Descrizione fisica 1 online resource (x, 83 pages) : illustrations
Altri autori (Persone) DouglasM. J (Michael J.)
Collana [NASA technical paper]
Soggetto topico Low speed
Composite materials
Impact tests
Indentation
Static tests
Mechanical properties
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910702452003321
Nettles A. T (Alan T.)  
[Marshall Space Flight Center, AL] : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , [2000]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
A damage tolerance comparison of composite hat-stiffened and honeycomb sandwich structure for launch vehicle interstage applications [[electronic resource] /] / A.T. Nettles
A damage tolerance comparison of composite hat-stiffened and honeycomb sandwich structure for launch vehicle interstage applications [[electronic resource] /] / A.T. Nettles
Autore Nettles A. T (Alan T.)
Pubbl/distr/stampa Huntsville, Ala. : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , [2011]
Descrizione fisica 1 online resource (vii, 39 pages) : illustrations (some color)
Collana NASA/TM
Soggetto topico Compressive strength
Impact strength
Honeycomb structures
Launch vehicles
Damage
Tolerances (mechanics)
Residual strength
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910701853303321
Nettles A. T (Alan T.)  
Huntsville, Ala. : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , [2011]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
The effects of compressive preloads on the compression-after-impact strength of carbon/epoxy / / A.T. Nettles and D.G. Lance
The effects of compressive preloads on the compression-after-impact strength of carbon/epoxy / / A.T. Nettles and D.G. Lance
Autore Nettles A. T (Alan T.)
Pubbl/distr/stampa [Washington, D.C.] : , : National Aeronautics and Space Administration, Office of Management, Scientific and Technical, Information Program, , 1992
Descrizione fisica 1 online resource (iv, 16 pages) : illustrations
Collana NASA technical paper
Soggetto topico Impact strength
Epoxy matrix composites
Prestressing
Strain distribution
Impact tests
Compression loads
Compressive strength
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707973403321
Nettles A. T (Alan T.)  
[Washington, D.C.] : , : National Aeronautics and Space Administration, Office of Management, Scientific and Technical, Information Program, , 1992
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
The effects of foam thermal protection system on the damage tolerance characteristics of composite sandwich structures for launch vehicles [[electronic resource] /] / A.T. Nettles, A.J. Hodge, and J.R. Jackson
The effects of foam thermal protection system on the damage tolerance characteristics of composite sandwich structures for launch vehicles [[electronic resource] /] / A.T. Nettles, A.J. Hodge, and J.R. Jackson
Autore Nettles A. T (Alan T.)
Pubbl/distr/stampa [Huntsville], Ala. : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , [2011]
Descrizione fisica 1 online resource (vii, 23 pages) : illustrations
Altri autori (Persone) HodgeA. J
JacksonJ. R
Collana NASA/TP
Soggetto topico Damage assessment
Launch vehicles
Thermal protection
Sandwich structures
Residual strength
Ares 1 launch vehicle
Composite structures
Composite materials
Impact damage
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910700761103321
Nettles A. T (Alan T.)  
[Huntsville], Ala. : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , [2011]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Hot/wet open hole compression strength of carbon/epoxy laminates for launch vehicle applications [[electronic resource] /] / A.T. Nettles
Hot/wet open hole compression strength of carbon/epoxy laminates for launch vehicle applications [[electronic resource] /] / A.T. Nettles
Autore Nettles A. T (Alan T.)
Pubbl/distr/stampa [Huntsville], Ala. : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , [2009]
Descrizione fisica 1 online resource (vii, 23 pages) : illustrations (some color)
Collana NASA/TM
Soggetto topico Epoxy matrix composites
Temperature effects
Compressive strength
Launch vehicles
Safety factors
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910700382303321
Nettles A. T (Alan T.)  
[Huntsville], Ala. : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , [2009]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
The impact response of carbon/epoxy laminates / / A.T. Nettles and A.J. Hodge
The impact response of carbon/epoxy laminates / / A.T. Nettles and A.J. Hodge
Autore Nettles A. T (Alan T.)
Pubbl/distr/stampa Marshall Space Flight Center, Alabama : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , November 1997
Descrizione fisica 1 online resource (viii, 165 pages) : illustrations
Collana NASA/TM
Soggetto topico Epoxy matrix composites
Laminates
Impact tests
Dynamic tests
Soggetto genere / forma Technical Memorandum
Soggetto non controllato Impact Phenomena
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910705766303321
Nettles A. T (Alan T.)  
Marshall Space Flight Center, Alabama : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , November 1997
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Normalization of impact energy by laminate thickness for compression after impact testing / / A.T. Nettles and S.M. Hromisin
Normalization of impact energy by laminate thickness for compression after impact testing / / A.T. Nettles and S.M. Hromisin
Autore Nettles A. T (Alan T.)
Pubbl/distr/stampa Huntsville, Alabama : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , 2013
Descrizione fisica 1 online resource (ix, 37 pages) : illustrations (some color)
Collana NASA/TP
Soggetto topico Laminates
Thickness
Impact strength
Compression loads
Mechanical properties
Impact tolerances
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910704629203321
Nettles A. T (Alan T.)  
Huntsville, Alabama : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , 2013
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Permeability testing of impacted composite laminates for use on reusable launch vehicles / / A.T. Nettles
Permeability testing of impacted composite laminates for use on reusable launch vehicles / / A.T. Nettles
Autore Nettles A. T (Alan T.)
Pubbl/distr/stampa MSFC, Alabama : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , February 2001
Descrizione fisica 1 online resource (v, 21 pages) : illustrations
Collana NASA/TM
Soggetto topico Laminates
Leakage
Permeability
Microcracks
Impact tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910706554403321
Nettles A. T (Alan T.)  
MSFC, Alabama : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , February 2001
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
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
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
Autore Nettles A. T (Alan T.)
Pubbl/distr/stampa Huntsville, Alabama : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , January 2022
Descrizione fisica 1 online resource (approximately 30 pages) : illustrations (some color)
Collana NASA/TM
Soggetto topico Composite materials
Sandwich structures
Carbon fibers
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910717163103321
Nettles A. T (Alan T.)  
Huntsville, Alabama : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , January 2022
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui

Data di pubblicazione