Maraging Steel C250 Round Bar is a high-grade, ultra-high-strength alloy extensively used in aerospace, military, and high-performance engineering applications. Meta Aerospace provides accurately engineered Maraging Steel C250 Round Bars for ensuring reliability, durability, and consistent performance in demanding environments.
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Maraging Steel C250 Round Bar is a nickel-based steel alloy that possesses a very good strength-to-toughness combination. As opposed to carbon steels, maraging steels such as C250 are hardened by the aging mechanism rather than by the level of carbon. Having a nominal composition of 18% nickel, complemented by cobalt, molybdenum, and titanium, the steel is heat-treatable to very high strength levels without compromising on ductility. It also exhibits outstanding weldability and dimensions stability in machining and forming.
One of the prominent benefits of C250 Round Bar of Maraging Steel is that it possesses a very high strength-to-weight ratio. It develops tensile strengths of over 240 ksi (1655 MPa) after aging, which is perfect for applications where the saving of weight is important. It also exhibits very little distortion upon heat treatment and hence is a preferred material for critical components of high accuracy. Fatigue resistance and resistance to corrosion further make it attractive for use in harsh environments in the long term.
Meta Aerospace is one of the reputed Maraging Steel C250 Round Bar Suppliers that provides rounds that meet international standards such as AMS 6512, MIL-S-46850, and ASTM A579. Each of the rounds passes strict quality inspections to meet tight tolerance, stable mechanical qualities, and surface finish for demanding applications. Meta Aerospace boasts facilities that can meet bulk orders without any degradation in quality or delivery schedule.
These bars play a critical role in the aerospace sector because of their high temperature oxidation resistance and strength.
As trustworthy C250 Round Bar Suppliers of Maraging Steel, Meta Aerospace provides global supply and supply-on-time solutions. Customers enjoy efficient logistics, correct material certification, and technical support in choosing the appropriate product for their project requirements.
For new construction or upgrading, our round bars of C250 provide the strength and performance that engineers require. We are also one of the most reliable Maraging Steel C250 Round Bar Stockists in the market. We reduce lead times for projects and procurement by having a comprehensive inventory in readiness for shipment. We supply round bars in a wide range of diameters and lengths, designed to suit the requirements of aircraft frames, tooling components, and mission-critical components.
Meta Aerospace is also among the top Maraging Steel C250 Round Bar Exporters, operating in a global network that includes North America, Europe, the Middle East, and Asia. We supply OEMs, defense contractors, and MROs that need high-performance materials on tight timelines. Export-grade bars are packaged for transit protection and include full traceability documentation.
Standard | AMS 6512, MIL-S-46850, ASTM A538 |
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Dimensions | DIN, EN, ASTM, JIS, ASME, BS, AISI |
Round Bar Size | Diameter: 3-~800mm |
Flat Bar Size | Thickness: 2 -100mm |
Width: 10 to 500mm | |
Square Bar Size | 4 to 100mm |
Tolerance | H8, H9, H10, H11, H12, H13K9, K10, K11, K12 or as per clients’ requirements |
Finish | Cold (bright) drawn, centreless ground, hot rolled, smooth turned, peeled, slit rolled edge, hot rolled annealed, Rough Turned, Bright, Polish, Grinding, Centreless Ground & Black |
Surface | Hot Rolled Pickled, Bright, Sand Blasting Finished, Cold Drawn, Hairline,Polished |
Condition | Hardened & tempered, annealed |
Technique | Cold Drawn, Hot Rolled, Forged Round Bar,Cold Rolled, Rod |
Processing | Bar cutting to 650mm |
Form | Rod, Round, Flat Bar, Square, Round Rod, Forging etc. |
Alloy Name | Trade Name | UNS No. | British Specs | American Specs | German Specs |
---|---|---|---|---|---|
Maraging 250 |
Udimar 250 Maraging C250 Vascomax C250 |
UNS K92890 | BS S162 |
AMS 6512 Bar MIL-S-46850 Type 3 |
Werkstoff 1.6359 |
Weight% | Ni | Co | Mn | Si | C | Al | Mo | S | P | Ti | Fe | Cr | Cu |
---|---|---|---|---|---|---|---|---|---|---|---|---|---|
C250 | 17.0 / 19.0 | 7.0 / 8.5 | 0.10 max | 0.10 max | 0.03 max | 0.05 / 0.15 | 4.6 / 5.2 | 0.010 max | 0.010 max | 0.3 / 0.5 | Bal | 0.50 | 0.50 |
Material | Condition | Ultimate Tensile (min) | Yield Strength (Min) | Elongation in 4D % (min) | Hardness | ||
---|---|---|---|---|---|---|---|
Mpa | Ksi | Mpa | Ksi | ||||
Alloy Maraging C250 | After Maraging heat treatment 900°F | 1758 | 255 | 1724 | 250 | 6 | ≥ 48 HRC |
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