Maraging steel sheet is a high-strength material sheet known for its toughness, weldability, and crack-resistant properties. It is made up of iron, nickel, cobalt, molybdenum, and low carbon. Parag Metal supplies high-quality maraging steel sheets to a wide range of industries. As a leading supplier of maraging steel sheets, we provide sheets that are strong, durable, and suitable for high-stress applications. These sheets are also corrosion resistant and can be heat treated to increase strength.
Our maraging steel sheets are available in the size 20mm x 1200 x 500. We also offer specialized sheets like shim sheets, perforated sheets, and B.Q. profiles. Finishes include cold rolled (CR), 2B, 2D, BA No(8), satin, and hot rolled (HR). Hardness levels available such as quarter hard, half hard, soft, hard, and spring hard—depending on your need.
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We offer Maraging Steel 250, 300, and 350 grades. Maraging Steel 250 Sheet has 1,700 MPa yield strength and suits parts that need weldability and toughness. Maraging Steel 300 Sheet, with 2,000 MPa yield strength, is often used in missile parts and rocket casings. Maraging Steel 350 Sheet is the strongest at 2,300 MPa and used in landing gear, high-strength bolts, and aerospace parts.
Every maraging steel sheet goes through strict quality checks and tests before delivery. Our sheets meet ASTM A 538 and ASTM A579 standards. We pack all products securely to avoid damage in transit. Reach out to get high-performance sheets built for strength and reliability.
Extremely high strength while maintaining toughness.
Excellent dimensional stability during heat treatment.
Good machinability despite high strength.
Superior corrosion resistance in certain grades.
High fatigue and impact resistance, ideal for critical applications.
Can be age-hardened to achieve precise mechanical properties.
Widely applied in rocket motor casings and missile parts for toughness and dimensional stability.
Used in tooling and dies for high precision and wear resistance.
Suitable for high-performance shafts and gears in heavy machinery.
Applied in nuclear reactor components for strength and resistance to radiation.
Effective in automotive high-strength parts like crankshafts and suspension components.
| Specification : | ASTM A538, AMS 6512, Mil-S-46850D, BS S162, DTD 5212, MSRR 6551, MAT 102, MIA 101 |
|---|---|
| Standard : | AMS, AMS, API |
| Size : | 20mm x 1200 x 500 |
| Specialize sheets : | Shim, Perforated Sheet, B. Q. Profile. |
| Finish : | Cold rolled sheet (CR), 2D, Hot rolled plate (HR), 2B, BA NO(8), SATIN (Met with Plastic Coated) |
| Hardness : | Quarter Hard, Soft, Hard, Half Hard, Spring Hard etc. |
| Grade : | Maraging Steel 250/ 300 / 350 (UNS-K92890, K93120, S35000) |



| STANDARD | UNS | Material No | AMS | ASTM | Mil-S | BS | DTD | MSRR |
|---|---|---|---|---|---|---|---|---|
| Maraging Steel | K92890, K93120, S35000 | – | 6512 | A538 | 46850D | S162 | 5212 | 6551 |
| 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 |
| Weight% | C | Si | Mn | S | P | Co | Ni | Mo | Ti | Al | Fe |
|---|---|---|---|---|---|---|---|---|---|---|---|
| Maraging 300 | 0.03 max | 0.10 max | 0.10 max | 0.010 max | 0.010 max | 8.0–9.5 | 18.0–19.0 | 4.6–5.2 | 0.55–0.80 | 0.05–0.15 | Bal |
| Weight% | Ni | Co | Mn | Si | C | B | P | S | Al | Mo | Ti | Zr |
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Maraging 350 | 18.50 | 12.0 | 0.10 max | 0.10 max | 0.03 max | 0.003 | 0.01 max | 0.01 max | 0.10 | 4.8 | 1.40 | 0.01 |
| 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 |
| Material | 0.2 % Yield Strength ksi | Ultimate Tensile Strength ksi | Elongation in 4D (%) | Reduction of Area % | Hardness Rc |
|---|---|---|---|---|---|
| Maraging 300, Solution Annealed 1500°F (816°C), 1hr, AC | 120 | 150 | 16 | 70 | 30 |
| Solution Annealed Plus Aged 900°F (482°C), 3 hrs AC | 280 | 290 | 8 | 40 | 52 |
| Material | 0.2 % Yield Strength ksi | Ultimate Tensile Strength ksi | Elongation in 4D (%) |
|---|---|---|---|
| Maraging 350 | 330 | 350 | 8 |
Size (in mm) | Size (in inches) |
|---|---|
3.40mm | .134″ |
3.18mm | .125″ |
4.75mm | .187″ |
3.96mm | .156″ |
7.92mm | .312″ |
6.35mm | .250″ |
12.7mm | .500″ |
9.53mm | .375″ |
19.1mm | .750″ |
15.9mm | .600″ |
25.4mm | 1″ |
22.2mm | .875″ |
31.8mm | 1.250″ |
28.6mm | 1.125″ |
44.5mm | 1.750″ |
38.1mm | 1.500″ |
63.5mm | 2.500″ |
50.8mm | 2″ |
76.2mm | 3″ |
| Tolerance over and under nominal thickness t (mm) | ||||||||||
|---|---|---|---|---|---|---|---|---|---|---|
| Width w (mm) | 2.5<t <4.5 | 4.5<t <6.0 | 6.0<t <8.0 | 8.0<t <10.0 | 10.0<t <12.5 | 12.5<t <16.0 | 16.0<t <20.0 | 20.0<t <25.0 | 25.0<t <30.0 | 30<t <40.0 |
| w < 1200 | 0.20 | 0.23 | 0.30 | 0.32 | 0.35 | 0.80 | 0.80 | 0.80 | 1.0 | 1.4 |
| 1200< w <1500 | 0.20 | 0.25 | 0.30 | 0.35 | 0.38 | 0.80 | 0.80 | 0.90 | 1.0 | 1.4 |
| 1500< w <1800 | 0.20 | 0.28 | 0.32 | 0.38 | 0.40 | 0.80 | 0.80 | 0.90 | 1.1 | 1.5 |
| 1800< w <2100 | 0.20 | 0.30 | 0.36 | 0.40 | 0.45 | 0.80 | 0.80 | 0.90 | 1.1 | 1.5 |
| 2100< w <2400 | 0.80 | 0.80 | 0.80 | 0.80 | 0.80 | 0.90 | 1.0 | 1.1 | 1.5 | |
| 2400< w <2700 | 0.80 | 0.80 | 0.80 | 0.80 | 0.90 | 1.0 | 1.1 | 1.3 | 1.7 | |
| 2700< w <3000 | 0.80 | 0.90 | 1.0 | 1.0 | 1.0 | 1.1 | 1.3 | 1.4 | 1.8 | |
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