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| Material Type | Key Properties | Typical Engine Application |
|---|---|---|
| Alloy Steel | High tensile strength (up to 200,000 psi), excellent fatigue resistance, cost-effective | Securing structural components like engine mounts and casing flanges |
| Stainless Steel | Chromium-rich (10-30%), corrosion and oxidation resistance, moderate strength | Fan section, external engine components, and areas exposed to moisture/salt |
| Nickel Alloy | Exceptional high-temperature strength (retains 80% strength at 1,800°F), creep resistance | Turbine blades, combustion chamber liners, and heat exchanger tubes |
| Titanium Alloy | High strength-to-weight ratio, corrosion resistance, low density | Lightweight structural components in the compressor section |
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