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 | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
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] | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
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] | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
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 | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
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] | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
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] | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
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 | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
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 | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
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 | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
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 | ||
| Lo trovi qui: Univ. Federico II | ||
| ||