Inconel® 2.4669 alloy X-750 wire 1.5-2.5mm N07750 nickel alloy (size : 2.5mm, length : 250 Meter (10.2kg))
- Do you need a different steel quality or dimensions? Please write to us. Our sales team makes an offer from stock program or delivery program :)
- Areas of application: components for gas turbines; combustion chamber of rocket engines; highly heat-resistant springs, screws and fasteners (up to 650 °C)
- electrical resistance 1.21 Ω mm²/m; Thermal conductivity 12 W/(m K).
- density 8.28 g/cm³; melting point 1430 °C;
- Didn't find the sizes you wanted? Just contact us! We are happy to help you with your request.

Length tolerance: +/-2mm
If you require alternative steel grades or custom dimensions, please contact us. Our sales team will offer you options from our stock or delivery program.
- Production time: 2-3 weeks.
- Preparation for dispatch: 2-3 business days.
- Delivery time: depends on the parcel service. Please refer to our FAQ for more details.
2.4669 is a hardenable nickel-chromium-iron alloy. It contains approximately 70% nickel and 15% chromium, with iron (about 7%) and titanium (around 2.5%) as main alloying components. Aluminium, niobium, cobalt, and manganese together make up about 4%. Alloy X-750 stands out for its excellent resistance to corrosion and oxidation, as well as its high strength at temperatures up to 700 °C.
Evek GmbH is your dependable supplier for 2.4669. Purchase premium nickel alloys at competitive prices.
Alloy X-750 is primarily used for manufacturing components for gas turbines and is also suitable for:
- Rocket engine combustion chambers;
- High-temperature springs, screws, and fasteners (up to 650 °C).
The key properties of 2.4669 include:
- Excellent resistance to corrosion and oxidation;
- High creep and heat resistance;
- Outstanding relaxation resistance.
Alloy X-750 is available in the Evek GmbH online store, along with a wide range of other nickel alloys at attractive prices.
- Type
- Wire
- material
- Nickel alloy
- operation area
- Components for gas turbines; combustion chamber of rocket engines; high-temperature resistant springs, screws and fasteners (up to 650 °C)
- Alloy
- C-276
- Thermal conductivity
- 12 W/(m-K)
- Electrical resistance
- 1.21 Ω mm²/m