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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 [[electronic resource] /] / A.J. Hodge, A.T. Nettles, and J.R. Jackson
| Comparison of open-hole compression strength and compression after impact strength on carbon fiber/epoxy laminates for the Ares I composite interstage [[electronic resource] /] / A.J. Hodge, A.T. Nettles, and J.R. Jackson |
| Author | Hodge A. J |
| Publication | [Huntsville], Ala. : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , [2011] |
| Physical description | 1 online resource (viii, 23 pages) : illustrations (some color) |
| Other authors (Person) |
NettlesA. T (Alan T.)
JacksonJ. R |
| Series statement | NASA/TP |
| Topical subject |
Compressive strength
Sandwich structures Carbon fibers Impact strength Damage Epoxy matrix composites Laminates Fiber composites |
| Format | Language material  |
| Bibliographic level | Monograph |
| Language | eng |
| Record Nr. | UNINA-9910700760803321 |
Hodge A. J
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| [Huntsville], Ala. : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , [2011] | ||
| Language material | ||
| You will find it: 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 |
| Author | Nettles A. T (Alan T.) |
| Publication | [Huntsville], Ala. : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , [2011] |
| Physical description | 1 online resource (vii, 23 pages) : illustrations |
| Other authors (Person) |
HodgeA. J
JacksonJ. R |
| Series statement | NASA/TP |
| Topical subject |
Damage assessment
Launch vehicles Thermal protection Sandwich structures Residual strength Ares 1 launch vehicle Composite structures Composite materials Impact damage |
| Format | Language material |
| Bibliographic level | Monograph |
| Language | eng |
| Record Nr. | UNINA-9910700761103321 |
|
Nettles A. T (Alan T.)
|
||
| [Huntsville], Ala. : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , [2011] | ||
| Language material | ||
| You will find it: Univ. Federico II | ||
| ||
Simplification of fatigue test requirements for damage tolerance of composite interstage launch vehicle hardware [[electronic resource] /] / A.T. Nettles, A.J. Hodge, and J.R. Jackson
| Simplification of fatigue test requirements for damage tolerance of composite interstage launch vehicle hardware [[electronic resource] /] / A.T. Nettles, A.J. Hodge, and J.R. Jackson |
| Author | Nettles A. T (Alan T.) |
| Publication | [Huntsville], Ala. : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , [2010] |
| Physical description | 1 online resource (27 pages) : illustrations |
| Other authors (Person) |
HodgeA. J
JacksonJ. R |
| Series statement | NASA/TP |
| Topical subject |
Composite materials
Compression loads Degradation Damage Fatigue (materials) Tolerances (mechanics) Failure |
| Format | Language material |
| Bibliographic level | Monograph |
| Language | eng |
| Record Nr. | UNINA-9910699653603321 |
|
Nettles A. T (Alan T.)
|
||
| [Huntsville], Ala. : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , [2010] | ||
| Language material | ||
| You will find it: Univ. Federico II | ||
| ||