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.

1101001.01.52.02.5Polypropylene (PP) — E 1.4 GPa · ρ 0.905 g/cm³Polyamide 6 (PA6, Nylon 6) — E 2.8 GPa · ρ 1.13 g/cm³Polycarbonate (PC) — E 2.4 GPa · ρ 1.2 g/cm³PEEK — E 3.6 GPa · ρ 1.3 g/cm³Polyethylene, high-density (HDPE) — E 1 GPa · ρ 0.95 g/cm³PVC, rigid (uPVC) — E 3 GPa · ρ 1.4 g/cm³Polystyrene (GPPS) — E 3.2 GPa · ρ 1.05 g/cm³Acrylic (PMMA) — E 3.1 GPa · ρ 1.19 g/cm³ABS — E 2.3 GPa · ρ 1.05 g/cm³PET — E 2.9 GPa · ρ 1.37 g/cm³Polyamide 66 (PA66, Nylon 66) — E 3.2 GPa · ρ 1.14 g/cm³PTFE (Teflon) — E 0.5 GPa · ρ 2.17 g/cm³PEI (Ultem) — E 3.2 GPa · ρ 1.27 g/cm³Epoxy (DGEBA, amine-cured) — E 3.45 GPa · ρ 1.2 g/cm³Polyester (unsaturated, cast) — E 3.2 GPa · ρ 1.2 g/cm³Vinyl ester — E 3.2 GPa · ρ 1.12 g/cm³Phenolic (phenol-formaldehyde) — E 3.5 GPa · ρ 1.28 g/cm³E-glass fiber — E 72.4 GPa · ρ 2.54 g/cm³Carbon fiber (T300) — E 230 GPa · ρ 1.76 g/cm³Aramid fiber (Kevlar 49) — E 131 GPa · ρ 1.44 g/cm³S-2 glass fiber — E 86.9 GPa · ρ 2.46 g/cm³Carbon fiber (AS4) — E 231 GPa · ρ 1.79 g/cm³Carbon fiber (IM7) — E 276 GPa · ρ 1.78 g/cm³Basalt fiber — E 89 GPa · ρ 2.67 g/cm³Flax fiber (natural) — E 58 GPa · ρ 1.5 g/cm³E-glass/epoxy UD lamina — E 39 GPa · ρ 2.1 g/cm³T300/5208 carbon/epoxy UD lamina — E 181 GPa · ρ 1.6 g/cm³AS4/3501-6 carbon/epoxy UD lamina — E 142 GPa · ρ 1.6 g/cm³Kevlar 49/epoxy UD lamina — E 80 GPa · ρ 1.38 g/cm³Boron/epoxy (B4/5505) UD lamina — E 204 GPa · ρ 2 g/cm³AS4/PEEK (APC-2) UD lamina — E 138 GPa · ρ 1.57 g/cm³density (g/cm³)E (GPa, log scale)
ThermoplasticsThermosetsFibersUD laminae (E₁)hover a point · click to open the material

Semi-crystalline commodity thermoplastic; low density, good chemical resistance, low Tg.

Density0.905 g/cm³
E1.4 GPa
Tensile strength34 MPa
Tg-10 °C

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Semi-crystalline engineering thermoplastic; strong and tough, moisture-sensitive properties.

Density1.13 g/cm³
E2.8 GPa
Tensile strength78 MPa
Tg50 °C

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Amorphous engineering thermoplastic; outstanding impact toughness and optical clarity.

Density1.2 g/cm³
E2.4 GPa
Tensile strength65 MPa
Tg147 °C

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Semi-crystalline high-performance thermoplastic; excellent thermal and chemical resistance.

Density1.3 g/cm³
E3.6 GPa
Tensile strength100 MPa
Tg143 °C

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Semi-crystalline commodity thermoplastic; tough, cheap, chemically inert — pipes, containers, cutting boards.

Density0.95 g/cm³
E1 GPa
Tensile strength27 MPa
Tg-120 °C

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Amorphous commodity thermoplastic; stiff, flame-resistant, economical — window frames, pipes, ducting.

Density1.4 g/cm³
E3 GPa
Tensile strength48 MPa
Tg82 °C

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Amorphous commodity thermoplastic; stiff, optically clear, brittle — cutlery, CD cases, foam insulation (as EPS).

Density1.05 g/cm³
E3.2 GPa
Tensile strength46 MPa
Tg100 °C

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Amorphous thermoplastic; the clearest common plastic — aircraft windows, aquariums, light guides.

Density1.19 g/cm³
E3.1 GPa
Tensile strength72 MPa
Tg105 °C

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Amorphous terpolymer; balanced stiffness and impact toughness — LEGO bricks, appliance housings, FDM printing.

Density1.05 g/cm³
E2.3 GPa
Tensile strength44 MPa
Tg105 °C

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Semi-crystalline polyester; drink bottles and textile fiber, crystallinity set by processing.

Density1.37 g/cm³
E2.9 GPa
Tensile strength60 MPa
Tg76 °C

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Semi-crystalline engineering thermoplastic; higher melting than PA6, same moisture sensitivity — gears, cable ties, under-hood parts.

Density1.14 g/cm³
E3.2 GPa
Tensile strength83 MPa
Tg60 °C

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Semi-crystalline fluoropolymer; lowest friction of any solid plastic, chemically inert, but soft and creep-prone.

Density2.17 g/cm³
E0.5 GPa
Tensile strength24 MPa
Tm327 °C

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Amorphous high-performance thermoplastic; strength and flame resistance at elevated temperature — aircraft interiors, sterilizable medical parts.

Density1.27 g/cm³
E3.2 GPa
Tensile strength105 MPa
Tg217 °C

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Standard structural thermoset matrix; good adhesion and dimensional stability. Properties vary with cure.

Density1.2 g/cm³
E3.45 GPa
Tensile strength70 MPa
Tg120 °C

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Economical thermoset matrix for glass-fiber boats, tanks, and panels; cures at room temperature with styrene.

Density1.2 g/cm³
E3.2 GPa
Tensile strength55 MPa
Tg75 °C

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Between polyester and epoxy in cost and performance; excellent corrosion resistance — chemical tanks, marine hulls.

Density1.12 g/cm³
E3.2 GPa
Tensile strength86 MPa
Tg120 °C

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The original synthetic plastic (Bakelite); chars instead of burning — aircraft interiors, brake pads, ablatives.

Density1.28 g/cm³
E3.5 GPa
Tensile strength50 MPa
Tg175 °C

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Standard reinforcement glass fiber; isotropic, economical, moderate stiffness.

Density2.54 g/cm³
E72.4 GPa
Tensile strength3450 MPa

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Standard-modulus PAN carbon fiber; transversely isotropic (axial values listed).

Density1.76 g/cm³
E230 GPa
Tensile strength3530 MPa

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High-stiffness aramid; excellent specific strength and damage tolerance, weak in compression.

Density1.44 g/cm³
E131 GPa
Tensile strength3620 MPa

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High-strength glass fiber; ~40% stronger and stiffer than E-glass — ballistic panels, pressure vessels, aerospace.

Density2.46 g/cm³
E86.9 GPa
Tensile strength4890 MPa

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Aerospace-workhorse standard-modulus PAN carbon fiber; the fiber in AS4/3501-6 and APC-2 laminae.

Density1.79 g/cm³
E231 GPa
Tensile strength4447 MPa

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Intermediate-modulus PAN carbon fiber; higher stiffness and strength than AS4 — primary aircraft structure.

Density1.78 g/cm³
E276 GPa
Tensile strength5516 MPa

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Fiber melt-spun from volcanic rock; between E-glass and S-glass in properties, good thermal resistance.

Density2.67 g/cm³
E89 GPa
Tensile strength2900 MPa

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Plant bast fiber; best stiffness-to-weight of common natural fibers, renewable and vibration-damping — sporting goods, interior panels.

Density1.5 g/cm³
E58 GPa
Tensile strength800 MPa

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Unidirectional lamina, Vf ≈ 0.55. Use with the laminate calculator.

Density2.1 g/cm³
E₁39 GPa
E₂8.6 GPa
G₁₂3.8 GPa

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Classic aerospace unidirectional lamina, Vf ≈ 0.70. Reference material for CLT examples.

Density1.6 g/cm³
E₁181 GPa
E₂10.3 GPa
G₁₂7.17 GPa

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Widely characterized aerospace unidirectional lamina, Vf ≈ 0.63. Reference dataset in Daniel & Ishai.

Density1.6 g/cm³
E₁142 GPa
E₂10.3 GPa
G₁₂7.2 GPa

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Aramid unidirectional lamina, Vf ≈ 0.60. Note the very low compressive strengths — aramid's known weakness.

Density1.38 g/cm³
E₁80 GPa
E₂5.5 GPa
G₁₂2.2 GPa

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Classic boron-fiber lamina, Vf ≈ 0.50; enormous compressive strength from the thick stiff fibers — repair patches, historic aircraft parts.

Density2 g/cm³
E₁204 GPa
E₂18.5 GPa
G₁₂5.59 GPa

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Thermoplastic-matrix carbon lamina, Vf ≈ 0.61; tough, weldable, recyclable — the reference thermoplastic composite.

Density1.57 g/cm³
E₁138 GPa
E₂10.2 GPa
G₁₂5.7 GPa

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Where do these material properties come from?

Every value carries the source it came from — a handbook, a supplier datasheet or a paper — together with the test method and the conditions it was measured at. Nothing here is an unattributed number, because a property without its conditions is not data you can design with.

See the sources →

Can I use these numbers for design?

They are typical room-temperature figures, and they are right for learning, comparison and early sizing. They are not design allowables: real structure is sized from statistically derived values measured on your own material and process, and a supplier datasheet always overrides a textbook figure.

Why allowables sit below the average →

Why does the same plastic show different numbers elsewhere?

Because grade, fillers, moisture content, temperature, strain rate and test standard all move the result, often by a lot. Nylon that has absorbed water is measurably less stiff than dry nylon. That is exactly why every value here is published with its method and conditions attached.

What is the difference between stiffness and strength?

Stiffness is how much a material resists being deformed — the slope of the stress-strain line, measured as modulus. Strength is the stress at which it finally fails. A material can be very stiff and still weak, or strong and quite flexible; they are independent choices.

Stress, strain and why things break →