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handbook of carbon, graphite, diamond and fullerenes

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102 Carbon, Graphite, Diamond, <strong>and</strong> Fullerenes<br />

.1500<br />

Refractory Alloys<br />

Sic<br />

Graphite -<br />

400 1000 2000 3000<br />

Temperature °C<br />

Figure 5.7. Specific strength as a function <strong>of</strong> temperature <strong>of</strong> <strong>graphite</strong> <strong>and</strong> other<br />

high-temperature materials. I 12 '<br />

The room-temperature transverse (flexural) strength <strong>of</strong> molded-<strong>graphite</strong><br />

grades varies between 10 <strong>and</strong> 100 MPa <strong>and</strong> its Young's modulus (also at room<br />

temperature) is between 5 <strong>and</strong> 10 GPa. These large variations are due to<br />

differences in raw materials <strong>and</strong> processing techniques. Flexural testing is<br />

described in detail in the test procedures listed in Table 5.3. In the more<br />

common three-point loading test, typical test specimens have a square cross<br />

section, 5.08 mm (0.200 in) or 3.18 mm (0.125 in) on the side. The support span<br />

is 3.05 mm (1.20 in) or 1.52 mm (0.60 in) for the larger <strong>and</strong> smaller test<br />

specimens, respectively. The strength is given by the following formula:<br />

where:<br />

S =<br />

S = flexural strength<br />

P = load at rupture<br />

L = support span<br />

b = specimen width<br />

d = specimen thickness! 2 !

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