The 2219 alloy is used in aerospace applications such as space booster and fuel tanks. The alloy is weldable and resistant to stress corrosion cracking . Its useful temperature range is -452° to 600°F. The alloy also has good fracture toughness.
Others | ||||||||||||||||
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Weight % | Si | Fe | Cu | Mn | Mg | Zn | Ti | V | Zr | Each | Total | Aluminium | ||||
Minimum | — | — | 5.8 | 0.2 | — | — | 0.02 | 0.05 | 0.10 | — | — | Remainder | ||||
Maximum | 0.20 | 0.30 | 6.8 | 0.4 | 0.02 | 0.25 | 0.10 | 0.15 | 0.25 | 0.05 | 0.15 |
Characteristics | English | Metric | |
---|---|---|---|
Nominal density
(68°F/20°C) |
0.103 lbs/in3 | 2.84 mg/m3 | |
Melting range | 1010°F-1190°F | 543°C-643°C | |
Specific heat
(212 °F/100°C) |
0.206 BTU/lb – °F | 864 J/KG- °K | |
Coefficient of thermal expansion | Linear
68°F – 212°F 20°C – 100°C |
12.5 micro in/in- °F | 22.5 micro in/in- °K |
Volumetric
68 ºF / 20 ºC |
3.62 x 10– 5 in .3/in.3 – ºF | 65 x 10-6 m3/m3 – ºK | |
T3, T3551 | 67 BTU/ft- hr – °F | 116 W/m – °K | |
T8, T851, T8511 | 75 BTU/ft- hr – °F | 130 W/m – °K | |
Electrical conductivity
(68°F/20°C) |
Equal Volume | T3, T3551 | 28% IACS |
T8, T851, T8511 | 30% IACS |
Temper | Tensile (.500” Dia. Speciman) | Hardness | Shear | Fatigue | Modulus | ||||||||
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Ultimate | Yield | Elongation/ 4D | Brinell 500 kg 10 mm | Ultimate shearing strength | Endurance limit-R.R.Moore type | Modulus of elasticity | |||||||
KSI | MPa | KSI | MPa | KSI | MPa | KSI | MPa | KSIx103 | Gpa | ||||
T-351 | 52 | 359 | 36 | 248 | 17 | 95 | — | — | — | — | 10.6 | 73.1 | |
T-851 | 66 | 455 | 51 | 352 | 10 | 125 | — | — | 15 | 103 | 10.6 | 73.1 | |
T-37 | 57 | 393 | 46 | 317 | 11 | — | — | — | 15 | 103 | 10.6 | 73.1 | |
T-87 | 69 | 476 | 57 | 393 | 10 | — | — | — | 15 | 103 | 10.6 | 73.1 |