The specific strength is a material's strength (force per unit area at failure) divided by its density. It is also known as the strength-to-weight ratio or strength/weight ratio. In fiber or textile applications, tenacity is the usual measure of specific strength. The SI unit for specific strength is (N/m2)/(kg/m3) or more commonly N·m/kg.
Another way to describe specific strength is breaking length, also known as self support length: the maximum length of a vertical column of the material (assuming a fixed cross-section) that could suspend its own weight when supported only at the top. For this measurement, the definition of weight is the force of gravity at the Earth's surface applying to the entire length of the material, not diminishing with height. This usage is more common with certain specialty fiber or textile applications.
The materials with the highest specific strengths are typically fibers such as carbon fiber, glass fiber and various polymers, and these are frequently used to make composite materials (e.g. carbon fiber-epoxy). These materials and others such as titanium, aluminium, magnesium and high strength steel alloys are widely used in aerospace and other applications where weight savings are worth the higher material cost.
Note that strength and stiffness are distinct. Both are important in design of efficient and safe structures.
Contents |
Material | Strength (MPa) |
Density (g/cm³) |
Specific Strength (kN·m/kg) |
Breaking length (km) |
source |
---|---|---|---|---|---|
Scifer steel wire | 5,500 | 7.87 | 706 | 71.2 | [1] |
Bainite | 2,500 | 7.87 | 321 | 32.4 | [1] |
1 μm iron whiskers | 14,000 | 7.87 | 1800 | 183 | [1] |
Concrete | 10 | 2.30 | 4.35 | 0.44 | |
Rubber | 15 | 0.92 | 16.3 | 1.66 | |
Brass | 580 | 8.55 | 67.8 | 6.91 | [2] |
Oak | 60 | 0.69 | 86.95 | 8.86 | [3] |
Balsa (axial load) | 73 | 0.14 | 521 | 53.2 | [4] |
Polypropylene | 80 | 0.90 | 88.88 | 9.06 | [5] |
Nylon | 78 | 1.13 | 69.0 | 7.04 | [6] |
Magnesium | 275 | 1.74 | 158 | 16.11 | [7] |
Aluminium alloy (3003-H14) | 600 | 2.70 | 222 | 22.65 | [8] |
Steel alloy | 2,000 | 7.86 | 254 | 25.93 | [8] |
Titanium alloy | 1,300 | 4.51 | 288 | 29.38 | [8] |
carbon-epoxy composite | 1240 | 1.58 | 785 | 80 | [9] |
Silicon carbide | 3,440 | 3.16 | 1,088 | 110 | [10] |
Glass fiber | 3,400 | 2.60 | 1,307 | 133 | [8] |
Basalt fiber | 4,840 | 2.70 | 1,790 | 182.7 | [11] |
Vectran | 2,900 | 1.40 | 2,071 | 211 | [8] |
Carbon fiber (AS4) | 4,300 | 1.75 | 2,457 | 250 | [8] |
Kevlar | 3,620 | 1.44 | 2,514 | 256 | [12] |
Spectra fiber | 3,510 | 0.97 | 3,619 | 369 | [13] |
Zylon | 5,800 | 1.54 | 3,766 | 384 | [14] |
Colossal carbon tube | 6,900 | .116 | 59,483 | 6,066 | [15] |
Carbon nanotube (see note below) | 62,000 | .037-1.34 | 46,268-N/A | 4,716-N/A | [16][17] |
spider silk | 1,400 | 1.31 | 1,069 | 109 |
The data of this table is from best cases, and has been established for giving a rough figure.
Since N·m/kg (the unit of specific strength) expands to (kg·m/s2)·m/kg or (m/s)2, a specific strength can also be understood as the square of a speed, hence represented by it square root, a speed. Further, the structural analysis for whether a particular material is strong enough for some purpose can sometimes be expressed in terms of comparing this speed to the speed of a relevant part of the structure. For example, a spinning cylindrical shell (as in an idealized flywheel or an idealized cylinder space ship) is only feasible if built of a material whose square root of specific strength is at least the speed at which the spinning shell moves.