Materials/Composites/Collections
Glass and composites
glass-and-compositesAbout glass and composites
Glass and fibre composites (borosilicate glass, fused silica, E-glass, carbon-fibre composite, aramid, FR-4): density, stiffness, strength and temperature limits with sources.
Glasses are hard, stiff and brittle, and they soften over a range of temperatures instead of melting at one. Fibre composites put strong fibres in a resin so the part is light and stiff along the fibres. Each value here names its grade, form and condition.
At a glance
- Highest density: E-glass fibre reaches 2.62 g/cm³. Lowest: SRC starts at 0.91 g/cm³. (9 of 10 grades have a sourced value.)
- Highest young's modulus: CFRP reaches 230 GPa. Lowest: SRC starts at 0.55 GPa. (7 of 10 grades have a sourced value.)
- Highest tensile strength: CFRP reaches 4,900 MPa. Lowest: SRC starts at 40 MPa. (5 of 10 grades have a sourced value.)
Ranges run across the conditions each source reports (temper, heat treatment, form), measured at room temperature where the source says so.
How they compare
The same measurements for every material in the collection. A range means the grade has values under several conditions; "at least" means the source gives a specified minimum. "no data" means no sourced value yet. For ranked tables, open a benchmark.
| Material | Density | Young's modulus | Tensile strength | Thermal conductivity | Thermal expansion | Service temperature |
|---|---|---|---|---|---|---|
| Borosilicate glassoptical and laboratory glass | 2.23 g/cm³ | no data | no data | 1.2 W/(m·K) | 3.25 ppm/K | no data |
| Fused silica (SiO2 glass)optical window and cover glass | 2.2 g/cm³ | 72.7 GPa | no data | 1.3 to 1.4 W/(m·K) | 0.55 ppm/K | 1,080 °C |
| E-glass fibrereinforcement fibre | 2.59 to 2.62 g/cm³ | 73 GPa | 2,600 MPa | no data | no data | no data |
| CFRPstructural composite | 1.3 to 1.8 g/cm³ | 11.7 to 230 GPa | 64 to 4,900 MPa | no data | 0.18 ppm/K | 121 °C |
| FR-4rigid circuit-board substrate, woven glass cloth bonded with epoxy resin | no data | no data | no data | 0.4 W/(m·K) | 13 to 230 ppm/K | no data |
| Kevlar para-aramid fibrehigh-strength fibre | 1.44 g/cm³ | 70.5 to 112 GPa | 2,920 to 3,040 MPa | no data | no data | no data |
| Nomexmeta-aramid fibre and paper for spacesuit layers, thermal blankets and honeycomb | 0.96 to 1.37 g/cm³ | no data | 340 to 2,960 MPa | 0.14 W/(m·K) | 18 ppm/K | 204 °C |
| Soda-lime glasswindow and container glass | 2.5 g/cm³ | 72 GPa | no data | 0.94 W/(m·K) | 9.5 ppm/K | 110 to 150 °C |
| Aluminosilicate glassdisplay and cover glass | 2.38 to 2.48 g/cm³ | 71.5 to 78 GPa | no data | 1.09 W/(m·K) | 31.7 to 81.4 x10^-7/C | no data |
| SRCstructural composite | 0.91 to 1.44 g/cm³ | 0.55 to 112 GPa | 40 to 3,000 MPa | no data | -4.9 ppm/K | 82.2 to 177 °C |
What these materials are made of
Composition by weight, as printed in the sources for each grade (the first constituents listed).
| Material | Main constituents |
|---|---|
| Borosilicate glass | SiO2 80% · B2O3 13% · Na2O or K2O 4% · Al2O3 2% |
| Fused silica (SiO2 glass) | Si 46.7% · O 53.3% |
| Nomex | C 70.6% · H 4.2% · N 11.8% · O 13.4% |
| Soda-lime glass | SiO2 72.6% · Na2O 13.9% · CaO 8.4% · MgO 3.9% · Al2O3 1.1% · cullet 20% |
| Aluminosilicate glass | SiO2 67% · Na2O 25% · Al2O3 8% |
Where they are used
| Use | Grades |
|---|---|
| Reflecting telescope primary mirror | Borosilicate glass |
| Hot and cold mirrors and dichroic filters | Borosilicate glass |
| Telescope mirror substrates | Borosilicate glass |
| Optical window, lens and mirror substrate | Fused silica (SiO2 glass) |
| Solar-cell cover glass | Fused silica (SiO2 glass) |
| Crewed spacecraft windows (Space Shuttle forward windows) | Fused silica (SiO2 glass) |
| Boats and vehicle parts laminated with E-glass roving fabric | E-glass fibre |
| Containers and tanks laminated with E-glass roving fabric | E-glass fibre |
| Space launcher structures | CFRP |
| Primary and secondary aircraft structures | CFRP |
| Prototype optical bench of graphite-epoxy | CFRP |
| Printed circuit board substrate | FR-4 |
| Computers and communication equipment | FR-4 |
| Printed circuit boards in general | FR-4 |
| Body armour and ballistic vests | Kevlar para-aramid fibre |
| Cut-resistant gloves and protective clothing | Kevlar para-aramid fibre |
When each grade fits
| Material | Best for | Weakest at |
|---|---|---|
| Borosilicate glass | Laboratory glassware and optics that must survive temperature swings, where a low thermal expansion matters more than cost | Higher working temperature and processing cost than soda-lime glass; the expansion coefficient and hazard data could not be checked in this run |
| Fused silica (SiO2 glass) | Optics that must stay stable across temperature swings: very low thermal expansion and transparency from the ultraviolet to the near infrared | Brittleness, and a damaged pane can fail suddenly under tensile stress; the fetched sources give no outgassing numbers |
| E-glass fibre | General reinforcement of polyester, epoxy and vinylester laminates, such as boats, vehicle parts and containers, which are the end uses HP Textiles lists for its E-glass roving fabrics | Chemical resistance is not its strong point: HP Textiles lists C-glass, ECR-glass and boron-free Advantex as the corrosion-resistant types, and no E-glass corrosion value was read in this run |
| CFRP | Stiffness and strength per unit mass in structures: 164 GPa at 0 degrees in unidirectional IM7/8552 laminate | Strength across the fibres: 64 MPa at 90 degrees in unidirectional IM7/8552, and the epoxy limits service to about 121 C |
| FR-4 | Standard printed circuit boards: 180 °C Tg and 60 min T260 for multilayer boards, as printed for Isola 370HR | Loss at high frequency and expansion above Tg: a Z-axis CTE of 230 ppm/°C above Tg, and a dissipation factor of 0.0210 at 2 GHz |
| Kevlar para-aramid fibre | Light, strong fibre for body armour, cut-resistant gear and ropes, where the fibre is shielded from sunlight | Ultraviolet light, which discolours it and cuts its mechanical strength; and low stiffness in compression |
| Nomex | Flame-resistant, high-temperature electrical and thermal insulation layers: continuous service to 220 °C and an LOI above 20.8 at 220 °C, as printed by DuPont | Atomic oxygen in low Earth orbit: an erosion yield of 1.41e-24 cm3/atom on MISSE 2 means surface loss in orbit. Strength also falls with UV exposure and with heat ageing: about 65 % of breaking strength is kept after 1000 h at 260 °C |
| Soda-lime glass | Windows and containers where low cost and wide availability matter more than thermal shock or alkali resistance | Resistance to sudden temperature changes (high thermal expansion) and to alkaline solutions (NGA: poor resistance to alkalis) |
| Aluminosilicate glass | Thin cover and display glass that is chemically strengthened, where hardness and a high softening point matter more than cost | Cost and processing: EAGLE XG has a working point of 1293 C, and strengthening needs a molten potassium salt bath (EAGLE XG data, Zeng et al. 2016) |
| SRC | Light, recyclable structures where one polymer family is wanted: UHMWPE SRC gives about 1.0 g/cm3 with 174.3 MPa along the fibres | Strength across the fibres: 7.7 MPa transverse against 174.3 MPa along them, and the polyolefin SRC softens near 135 C in its unfilled matrix |