Kevlar 49/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.

Kevlar 49/epoxy UD lamina in fullT300/5208 carbon/epoxy UD lamina in full← All materials
PropertyKevlar 49/epoxy UD laminaT300/5208 carbon/epoxy UD laminaDifference
Density1.38 g/cm³1.6 g/cm³T300/5208 carbon/epoxy UD lamina — 16% higher
E₁ (longitudinal)80 GPa181 GPaT300/5208 carbon/epoxy UD lamina — 2.3× higher
E₂ (transverse)5.5 GPa10.3 GPaT300/5208 carbon/epoxy UD lamina — 87% higher
G₁₂ (in-plane shear)2.2 GPa7.17 GPaT300/5208 carbon/epoxy UD lamina — 3.3× higher
ν₁₂ (major Poisson)0.34 0.28 Kevlar 49/epoxy UD lamina — 21% higher
Xt (long. tension)1400 MPa1500 MPaT300/5208 carbon/epoxy UD lamina — 7% higher
Xc (long. compression)235 MPa1500 MPaT300/5208 carbon/epoxy UD lamina — 6.4× higher
Yt (transv. tension)12 MPa40 MPaT300/5208 carbon/epoxy UD lamina — 3.3× higher
Yc (transv. compression)53 MPa246 MPaT300/5208 carbon/epoxy UD lamina — 4.6× higher
S (in-plane shear)34 MPa68 MPaT300/5208 carbon/epoxy UD lamina — 2.0× 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.