AS4/3501-6 carbon/epoxy UD lamina vs T300/5208 carbon/epoxy UD lamina

Every value below is a typical room-temperature figure with its source, test method and conditions — the same dataset that drives the calculators.

AS4/3501-6 carbon/epoxy UD lamina in fullT300/5208 carbon/epoxy UD lamina in full← All materials
PropertyAS4/3501-6 carbon/epoxy UD laminaT300/5208 carbon/epoxy UD laminaDifference
Density1.6 g/cm³1.6 g/cm³identical
E₁ (longitudinal)142 GPa181 GPaT300/5208 carbon/epoxy UD lamina — 27% higher
E₂ (transverse)10.3 GPa10.3 GPaidentical
G₁₂ (in-plane shear)7.2 GPa7.17 GPaAS4/3501-6 carbon/epoxy UD lamina — 0% higher
ν₁₂ (major Poisson)0.27 0.28 T300/5208 carbon/epoxy UD lamina — 4% higher
Xt (long. tension)2280 MPa1500 MPaAS4/3501-6 carbon/epoxy UD lamina — 52% higher
Xc (long. compression)1725 MPa1500 MPaAS4/3501-6 carbon/epoxy UD lamina — 15% higher
Yt (transv. tension)57 MPa40 MPaAS4/3501-6 carbon/epoxy UD lamina — 43% higher
Yc (transv. compression)228 MPa246 MPaT300/5208 carbon/epoxy UD lamina — 8% higher
S (in-plane shear)76 MPa68 MPaAS4/3501-6 carbon/epoxy UD lamina — 12% higher
  • Daniel & Ishai, Engineering Mechanics of Composite Materials, 2nd ed.
  • Tsai & Hahn, Introduction to Composite Materials, 1980

Typical room-temperature values for learning and preliminary design; grades vary widely and a supplier datasheet always overrides a textbook figure. Confirm against the datasheet before design work.