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. 2016 Dec 28;11(12):e0168218. doi: 10.1371/journal.pone.0168218

Table 1. Strength-to-modulus and density ratios for commonly used materials in the space industry.

Material Material Properties Property Ratios
Sy (GPa) E (GPa) ρ (g/cm3) Sy/() *1000 Sy/E *1000 Sy/ρ *1000
Vitreloy 1 (metallic glass) 1.8 95 ∼5.8 3.27 18.95 310.3
Al alloy 7050 ∼0.44 70.3 2.82 2.22 6.26 156
Al alloy 7075 ∼0.45 71 2.8 2.26 6.34 160.7
Ti-6Al-4V 0.825 110 4.43 1.70 7.52 186.7
Elgiloy (85% HT) 2.12 189.6 8.30 1.35 11.2 255
Inconel 718 (Nickel alloy) 1.034 202.7 4.43 1.15 5.10 233
MP35N (65%) 1.62 234.8 8.43 0.82 6.90 192
Stainless 17-7TH 1050 1.034 200 7.64 0.68 5.17 135
Stainless 15-5PH H1025 0.986 196.5 7.83 0.64 5.02 126
Invar 36 (cold rolled) 0.679 148 8.05 0.57 4.59 84.3
Tantalum (UNS R05400) 0.22 185 16.6 0.07 1.19 13.2
Copper alloy (C10200-060) 0.0758 117.2 8.94 0.072 0.65 8.5
Teflon PTFE film 0.018 0.5 2.2 16.4 36 8.2
Mylar A film 0.103 3.8 1.4 19.4 27 73.5
Kapton HN film 0.07 2.8 1.42 17.6 25 49
Teflon FEP film 0.012 0.48 2.15 11.6 25 5.6
Tefzel film 0.006 1.2 1.7 3 5 3.5
Butyl rubber 0.014 3.4 0.92 4.5 4.1 15