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Comparison

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Property T300/F550 ply transverse-strength ICAN estimates (NASA)
T6T 262-12F 550 source prepreg system represented by ICAN model 6 | continuous-fiber ply model for a source [+-45_2]s prepreg laminate
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.
Young's modulus
Not listed
Not listed for this material record, condition, or selected unit system.
Shear modulus
Not listed
Not listed for this material record, condition, or selected unit system.
Poisson's ratio
Not listed
Not listed for this material record, condition, or selected unit system.
Yield strength
Not listed
Not listed for this material record, condition, or selected unit system.
Tensile strength
97.0 MPa
Transverse tensile strength
Computational Predicted Screening
source material T6T 262-12F 550, high-tenacity Union Carbide T300-6000 fiber / Hexcel F550 resin, 60 vol% fiber; ICAN material designation 6; use temperature 21 degC; cure temperature 120 degC
186.0 MPa
Transverse tensile strength at -155 degC
Computational Predicted Screening
source material T6T 262-12F 550, high-tenacity Union Carbide T300-6000 fiber / Hexcel F550 resin, 60 vol% fiber; ICAN material designation 6; use temperature -155 degC; cure temperature 120 degC
110.0 MPa
Transverse tensile strength at 95 degC
Computational Predicted Screening
source material T6T 262-12F 550, high-tenacity Union Carbide T300-6000 fiber / Hexcel F550 resin, 60 vol% fiber; ICAN material designation 6; use temperature 95 degC; cure temperature 120 degC
Elongation at break
Not listed
Not listed for this material record, condition, or selected unit system.
Maximum service temperature
Not listed
Not listed for this material record, condition, or selected unit system.