Materials
Compare Materials
Compare candidate materials with unit-aware values and condition metadata.
| Property |
T300/913C UD tape lamina model inputs (NASA/WWFE reference)
cured T300 carbon-fiber/913C-resin unidirectional tape lamina model | unidirectional tape lamina (0-degree tape in the analyzed structure)
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|---|---|
| Density |
Not listed
Not listed for this material record, condition, or selected unit system.
|
| Thermal conductivity |
Not listed
Not listed for this material record, condition, or selected unit system.
|
| Specific heat capacity |
Not listed
Not listed for this material record, condition, or selected unit system.
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| Young's modulus |
Not listed
Not listed for this material record, condition, or selected unit system.
|
| Shear modulus |
5.5 GPa
In-plane shear modulus
Source Reported Model Input Screening
T300/913C unidirectional tape lamina; room-temperature state is not explicitly stated; parameter used by the NASA progressive-failure analysis
|
| Poisson's ratio |
Not listed
Not listed for this material record, condition, or selected unit system.
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| Yield strength |
Not listed
Not listed for this material record, condition, or selected unit system.
|
| Tensile strength |
1500.0 MPa
Longitudinal tensile strength
Source Reported Model Input Screening
T300/913C unidirectional tape lamina; room-temperature state is not explicitly stated; parameter used by the NASA progressive-failure analysis
27.0 MPa
Transverse tensile strength
Source Reported Model Input Screening
T300/913C unidirectional tape lamina; room-temperature state is not explicitly stated; parameter used by the NASA progressive-failure analysis
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| Elongation at break |
Not listed
Not listed for this material record, condition, or selected unit system.
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| Maximum service temperature |
Not listed
Not listed for this material record, condition, or selected unit system.
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