2195-T8 represents the third generation of aluminum-lithium alloys, specifically engineered for aerospace applications where weight reduction and cryogenic performance are critical. This alloy has become the incumbent material for space launch vehicle fuel tanks, including NASA's Space Launch System (SLS) and commercial vehicles like SpaceX's Falcon 9.
The 'T8' temper designation indicates solution heat treatment followed by cold working and artificial aging. This thermomechanical processing creates a fine dispersion of T1 (Al2CuLi) precipitates that provide exceptional strength-to-weight ratios. For aerospace manufacturers selling on Alibaba.com, understanding these specifications is essential when communicating with international buyers who require mill certificates and chemical analysis reports.
2195-T8 Mechanical Properties: Room Temperature vs Cryogenic Performance
| Property | Room Temperature | 77K (Liquid Nitrogen) | 20K (Liquid Hydrogen) |
|---|---|---|---|
| Ultimate Tensile Strength (MPa) | 580-620 | 720-750 | 859 |
| Yield Strength 0.2% (MPa) | 540-570 | 650-680 | 724 |
| Elongation (%) | 8-11 | 10-13 | 11-14 |
| Density (g/cm³) | 2.70 | 2.70 | 2.70 |
| Elastic Modulus (GPa) | 76-78 | 82-85 | 88-91 |
The cryogenic performance characteristics are particularly noteworthy. At 20K temperatures (liquid hydrogen storage), 2195-T8 exhibits a 39.9% increase in ultimate tensile strength compared to room temperature values. This phenomenon occurs because dislocation density increases from 2×10¹⁴ m⁻² to 5×10¹⁴ m⁻² at cryogenic temperatures, and multiple slip systems activate more uniformly, enhancing strength without catastrophic brittleness [3].

