Side-by-side summary.
Inconel 718
Precipitation-hardened nickel superalloy. 1035 MPa yield strength. Service to 650°C. Aerospace workhorse — rocket engines, jet engine hot section, high-stress + temperature applications.
Hastelloy C-276
Solid-solution nickel-molybdenum-chromium alloy. 355 MPa yield. Exceptional corrosion resistance to 1100°C. Chemical processing standard — handles aggressive chemistries other alloys cannot.
Feature-by-feature breakdown.
| Attribute | Inconel 718 | Hastelloy C-276 |
|---|---|---|
| Nickel content | 50-55% | 57% |
| Main alloying | Fe, Cr, Mo, Nb, Ti, Al | Mo, Cr, W, Fe |
| Yield strength | 1035 MPa (STA) | 355 MPa (annealed) |
| Hardening mechanism | Precipitation | Solid solution |
| Service temperature | 650°C (aged) | 1100°C (short-term) |
| Oxidation resistance | Good | Excellent |
| HCl resistance | Poor | Excellent |
| H2SO4 resistance | Moderate | Excellent |
| Chloride pitting (PREN) | ~50 | ~65 |
| Cost per kg | $50-80 | $60-100 |
| Machinability | Difficult (work hardening) | Difficult |
| Weldability | Good (post-weld age) | Excellent |
When to choose each.
Choose Inconel 718 when:
Choose Hastelloy C-276 when:
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