
Inconel X-750 (UNS N07750 / W.Nr. 2.4669) is a precipitation-hardenable nickel-chromium superalloy engineered for high strength, creep-rupture resistance, and corrosion resistance at elevated temperatures up to 700°C (1300°F). It retains useful mechanical properties down to cryogenic temperatures and is widely used in springs, gas turbine components, rocket engines, and nuclear reactors.
No chemical symbols included; values represent standard nominal weight percentages according to ASTM B637:
| Element | Nominal Content (%) | Min (%) | Max (%) |
| Nickel (plus Cobalt) | Balance (~73.0) | 70.0 | â |
| Chromium | 15.5 | 14.0 | 17.0 |
| Iron | 7.0 | 5.0 | 9.0 |
| Titanium | 2.5 | 2.25 | 2.75 |
| Aluminum | 0.7 | 0.40 | 1.00 |
| Niobium (plus Tantalum) | 1.0 | 0.70 | 1.20 |
| Manganese | â | â | 1.00 |
| Silicon | â | â | 0.50 |
| Copper | â | â | 0.50 |
| Carbon | â | â | 0.08 |
| Sulfur | â | â | 0.01 |
Density: 8.28 grams per cubic centimeter
Melting Range: 1395 to 1425 degrees Celsius
Ultimate Tensile Strength: 1100 to 1280 Megapascals
Yield Strength (0.2% Offset): 730 to 860 Megapascals
Elongation at Break: 20 to 25 percent
Hardness: 30 to 40 Rockwell C
Maximum Service Temperature: 700 degrees Celsius (higher for lower stress applications)
Scrap Grade Classification: Premium Vacuum Induction Melting (VIM) / Air Induction Melting (AIM) charge material.
Foundry Forms: Wire scrap, helical spring solids, turbine bolts, sheet cutoffs, ring forgings, and clean turnings/borings.
Quality Requirements: Must be kept strictly separate from non-titanium nickel alloys to preserve the age-hardening titanium-aluminum ratio. Scrap must be free of grease, heavy oxides, plating, solder, and free-machining elements before vacuum or induction remelting.
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