Materials Database
Every value carries its source, test method, and conditions. Select up to four materials to compare here, browse the head-to-head comparisons — or contribute a material.
The classic Ashby picture: stiffness against density. Up and to the left is light and stiff — notice where the fibers and laminae sit relative to the neat polymers.
Semi-crystalline commodity thermoplastic; low density, good chemical resistance, low Tg.
| Density | 0.905 g/cm³ |
| E | 1.4 GPa |
| Tensile strength | 34 MPa |
| Tg | -10 °C |
open the material for full provenance
Semi-crystalline engineering thermoplastic; strong and tough, moisture-sensitive properties.
| Density | 1.13 g/cm³ |
| E | 2.8 GPa |
| Tensile strength | 78 MPa |
| Tg | 50 °C |
open the material for full provenance
Amorphous engineering thermoplastic; outstanding impact toughness and optical clarity.
| Density | 1.2 g/cm³ |
| E | 2.4 GPa |
| Tensile strength | 65 MPa |
| Tg | 147 °C |
open the material for full provenance
Semi-crystalline high-performance thermoplastic; excellent thermal and chemical resistance.
| Density | 1.3 g/cm³ |
| E | 3.6 GPa |
| Tensile strength | 100 MPa |
| Tg | 143 °C |
open the material for full provenance
Semi-crystalline commodity thermoplastic; tough, cheap, chemically inert — pipes, containers, cutting boards.
| Density | 0.95 g/cm³ |
| E | 1 GPa |
| Tensile strength | 27 MPa |
| Tg | -120 °C |
open the material for full provenance
Amorphous commodity thermoplastic; stiff, flame-resistant, economical — window frames, pipes, ducting.
| Density | 1.4 g/cm³ |
| E | 3 GPa |
| Tensile strength | 48 MPa |
| Tg | 82 °C |
open the material for full provenance
Amorphous commodity thermoplastic; stiff, optically clear, brittle — cutlery, CD cases, foam insulation (as EPS).
| Density | 1.05 g/cm³ |
| E | 3.2 GPa |
| Tensile strength | 46 MPa |
| Tg | 100 °C |
open the material for full provenance
Amorphous thermoplastic; the clearest common plastic — aircraft windows, aquariums, light guides.
| Density | 1.19 g/cm³ |
| E | 3.1 GPa |
| Tensile strength | 72 MPa |
| Tg | 105 °C |
open the material for full provenance
Amorphous terpolymer; balanced stiffness and impact toughness — LEGO bricks, appliance housings, FDM printing.
| Density | 1.05 g/cm³ |
| E | 2.3 GPa |
| Tensile strength | 44 MPa |
| Tg | 105 °C |
open the material for full provenance
Semi-crystalline polyester; drink bottles and textile fiber, crystallinity set by processing.
| Density | 1.37 g/cm³ |
| E | 2.9 GPa |
| Tensile strength | 60 MPa |
| Tg | 76 °C |
open the material for full provenance
Semi-crystalline engineering thermoplastic; higher melting than PA6, same moisture sensitivity — gears, cable ties, under-hood parts.
| Density | 1.14 g/cm³ |
| E | 3.2 GPa |
| Tensile strength | 83 MPa |
| Tg | 60 °C |
open the material for full provenance
Semi-crystalline fluoropolymer; lowest friction of any solid plastic, chemically inert, but soft and creep-prone.
| Density | 2.17 g/cm³ |
| E | 0.5 GPa |
| Tensile strength | 24 MPa |
| Tm | 327 °C |
open the material for full provenance
Amorphous high-performance thermoplastic; strength and flame resistance at elevated temperature — aircraft interiors, sterilizable medical parts.
| Density | 1.27 g/cm³ |
| E | 3.2 GPa |
| Tensile strength | 105 MPa |
| Tg | 217 °C |
open the material for full provenance
Standard structural thermoset matrix; good adhesion and dimensional stability. Properties vary with cure.
| Density | 1.2 g/cm³ |
| E | 3.45 GPa |
| Tensile strength | 70 MPa |
| Tg | 120 °C |
open the material for full provenance
Economical thermoset matrix for glass-fiber boats, tanks, and panels; cures at room temperature with styrene.
| Density | 1.2 g/cm³ |
| E | 3.2 GPa |
| Tensile strength | 55 MPa |
| Tg | 75 °C |
open the material for full provenance
Between polyester and epoxy in cost and performance; excellent corrosion resistance — chemical tanks, marine hulls.
| Density | 1.12 g/cm³ |
| E | 3.2 GPa |
| Tensile strength | 86 MPa |
| Tg | 120 °C |
open the material for full provenance
The original synthetic plastic (Bakelite); chars instead of burning — aircraft interiors, brake pads, ablatives.
| Density | 1.28 g/cm³ |
| E | 3.5 GPa |
| Tensile strength | 50 MPa |
| Tg | 175 °C |
open the material for full provenance
Standard reinforcement glass fiber; isotropic, economical, moderate stiffness.
| Density | 2.54 g/cm³ |
| E | 72.4 GPa |
| Tensile strength | 3450 MPa |
open the material for full provenance
Standard-modulus PAN carbon fiber; transversely isotropic (axial values listed).
| Density | 1.76 g/cm³ |
| E | 230 GPa |
| Tensile strength | 3530 MPa |
open the material for full provenance
High-stiffness aramid; excellent specific strength and damage tolerance, weak in compression.
| Density | 1.44 g/cm³ |
| E | 131 GPa |
| Tensile strength | 3620 MPa |
open the material for full provenance
High-strength glass fiber; ~40% stronger and stiffer than E-glass — ballistic panels, pressure vessels, aerospace.
| Density | 2.46 g/cm³ |
| E | 86.9 GPa |
| Tensile strength | 4890 MPa |
open the material for full provenance
Aerospace-workhorse standard-modulus PAN carbon fiber; the fiber in AS4/3501-6 and APC-2 laminae.
| Density | 1.79 g/cm³ |
| E | 231 GPa |
| Tensile strength | 4447 MPa |
open the material for full provenance
Intermediate-modulus PAN carbon fiber; higher stiffness and strength than AS4 — primary aircraft structure.
| Density | 1.78 g/cm³ |
| E | 276 GPa |
| Tensile strength | 5516 MPa |
open the material for full provenance
Fiber melt-spun from volcanic rock; between E-glass and S-glass in properties, good thermal resistance.
| Density | 2.67 g/cm³ |
| E | 89 GPa |
| Tensile strength | 2900 MPa |
open the material for full provenance
Plant bast fiber; best stiffness-to-weight of common natural fibers, renewable and vibration-damping — sporting goods, interior panels.
| Density | 1.5 g/cm³ |
| E | 58 GPa |
| Tensile strength | 800 MPa |
open the material for full provenance
Unidirectional lamina, Vf ≈ 0.55. Use with the laminate calculator.
| Density | 2.1 g/cm³ |
| E₁ | 39 GPa |
| E₂ | 8.6 GPa |
| G₁₂ | 3.8 GPa |
open the material for full provenance
Classic aerospace unidirectional lamina, Vf ≈ 0.70. Reference material for CLT examples.
| Density | 1.6 g/cm³ |
| E₁ | 181 GPa |
| E₂ | 10.3 GPa |
| G₁₂ | 7.17 GPa |
open the material for full provenance
Widely characterized aerospace unidirectional lamina, Vf ≈ 0.63. Reference dataset in Daniel & Ishai.
| Density | 1.6 g/cm³ |
| E₁ | 142 GPa |
| E₂ | 10.3 GPa |
| G₁₂ | 7.2 GPa |
open the material for full provenance
Aramid unidirectional lamina, Vf ≈ 0.60. Note the very low compressive strengths — aramid's known weakness.
| Density | 1.38 g/cm³ |
| E₁ | 80 GPa |
| E₂ | 5.5 GPa |
| G₁₂ | 2.2 GPa |
open the material for full provenance
Classic boron-fiber lamina, Vf ≈ 0.50; enormous compressive strength from the thick stiff fibers — repair patches, historic aircraft parts.
| Density | 2 g/cm³ |
| E₁ | 204 GPa |
| E₂ | 18.5 GPa |
| G₁₂ | 5.59 GPa |
open the material for full provenance
Thermoplastic-matrix carbon lamina, Vf ≈ 0.61; tough, weldable, recyclable — the reference thermoplastic composite.
| Density | 1.57 g/cm³ |
| E₁ | 138 GPa |
| E₂ | 10.2 GPa |
| G₁₂ | 5.7 GPa |
open the material for full provenance