X750 Sheet, Coil - AMS 5598, AMS 5542
Inconel Alloy® X-750 is a nickel-chromium austenitic alloy similar to Alloy 600 but made precipitation-hardenable by additions of aluminum and titanium. It has good resistance to corrosion and oxidation along with high tensile and creep-rupture properties at high temperatures to 1300°F (700°C). Extended applications that require high strength at temperatures beyond 1100°F (593°C) may require a solution treatment, with air cooling between intermediate and final aging.
- Inventory & Specs
- Chemical Composition
- Physical Properties
- Mechanical Properties
- Datasheet
- Additional Info
Inventory Size Ranges for X750
| Type | Thickness | AMS Standards | UNS | Get a Quote |
|---|---|---|---|---|
| Coil | 0.0250" - 0.0680" | AMS 5598, AMS 5542 | UNS N07750 | Get a Quote |
| Sheet | 0.0250" - 0.0680" | AMS 5598, AMS 5542 | UNS N07750 | Get a Quote |
| Precision Reroll Strip | 0.0008" - 0.015" | Get a Quote |
Not finding what you are looking for? Connect with our specialty metals sourcing group.
Characteristics of X750
This material has excellent relaxation resistance and is non-magnetic. It has enhanced elevated temperature strength properties to 1300ºF (700°C) and oxidation resistance to 1800ºF (983˚C). Inconel® X-750 is resistant to a wide variety of industrial corrosives under both oxidizing and reducing conditions. This alloy also has excellent resistance to chloride stress corrosion cracking in the fully age hardened condition.
Working with X750
Nickel Alloy X-750 displays excellent workability including machinability and welding. It is precipitation hardenable.
Other industry standards we comply with:
- PWA-LCS
- GE Aircraft Engine (GT193)
- GE Aviation S-SPEC-35 AeDMS S-400
- RR SABRe Edition 2
- DFARS Compliant
- W.Nr 2.4669
Common Trade Names
- ATI X-750 (™ Allegheny Technologies)
- Inconel X750 (® Special Metals)
- Alloy X 750
- Inconel® X-750
Industry Applications for X750
- Gas turbines discs, thrust reversers, wheels and ducts
- Aircraft structures
- Rocket engines
- Nuclear reactors
- Heat treat fixtures
- Cryogenic vessels, springs, and fasteners
- Exhaust valves of diesel engines
Chemical Composition
| Element | Min | Max | |
|---|---|---|---|
| Ni/Co | Nickel + Cobalt | 70.0 | |
| Cr | Chromium | 14.0 | 17.0 |
| Fe | Iron | 5.0 | 9.0 |
| Ti | Titanium | 2.25 | 2.75 |
| Al | Aluminum | 0.4 | 1.0 |
| No/Ta | Nobelium & Tantalum | 0.7 | 1.2 |
| Si | Silicon | 0.50 | |
| S | Sulfur | 0.01 | |
| Cu | Copper | 0.50 | |
| C | Carbon | 0.08 | |
| Co | Cobalt | 1.00 | |
Physical Properties
| Property | Value |
|---|---|
| Density, lb/in³ | 0.299 |
| Melting Range | 2540-2600°F, 1395-1425°C |
| Curie Temperature | -225°F as hot-rolled -193 triple-heat-treated (2100°F/2 hr, A.C., +1500°F/24 hr, A.C. + 1300°F/20 hr, A.C.) |
| Magnetic Permeability | 70°F, 200H, as hot rolled 1.0020 1.0035 triple-heat-treated (2100°F/2 hr, A.C., +1500°F/24 hr, A.C., +1300°F/20 hr, A.C.) |
| Emissivity Oxidized Surface | 600°F 0.895, 2000°F 0.925 |
| Linear Contraction During Precipitation Treatment | 1300°F/20 hr), in/in Hot-rolled 0.00044, 20% Cold-rolled 0.00052, Annealed 0.00026 |
Mechanical Properties
| Property | Value |
|---|---|
Ultimate Tensile Strength, ksi | 120 |
.02% Yield Strength, ksi | 60 |
Elongation, % | 30 |
| Specification | Value |
|---|---|
AMS 5541 | 1300°F/20 hr., AC (Constant-temperature precipitation treatment). |
AMS 5598 | 1350°F/8 hr., FC to 1150°F, Hold at 1150°F for total precipitation-treating time of 18 hr., AC (Furnace-cool precipitation treatment). |