Maraging 250 steel Maraging 250

Fe-based alloy with nominal Ni 18.50, Co 7.50, Mo 4.80, Ti 0.40, Al 0.10 (SSA nominal, wt %)

Also known as UNS K92890, EN 1.6359, EN name X2NiCoMo18-8-5, BS S162, AMS 6512, ASTM A538 · 1 more

Maraging 250 steel is an 18% nickel, cobalt-strengthened steel (C-type) that is aged at a low temperature to reach its strength.

10 sources · Updated 2026-11-01 · CC BY 4.0

Evidence level

2 of 5

Lab-measured

Strength

240 ksi

Machinability before aging

30 to 35 HRC

Density

8.0 to 8.1 g/cm3

Recipe, share of the weight

  • Ni not statedNickel
  • Co not statedCobalt
  • Mo not statedMolybdenum
  • Ti not statedTitanium
  • Al not statedAluminium
  • Fe not statedIron

Best for

Ultra-high-strength structural parts that are machined soft and then aged, such as rocket motor cases and landing gear components

Weakest at

Corrosion behaviour is not documented in any source we hold, and the sources give properties that depend on bar size, test direction and aging cycle

Risk at a glance

  • People None found. No alloy hazard entry found
  • If it fails Moderate. Properties depend on the aging cycle
  • Corrosion No data. No corrosion data recorded

Quick facts: Maraging 250

Key properties of Maraging 250
PropertyValueBasis
Density8 to 8.1 g/cm³1 sourced value
Yield strengthat least 1,655 MPa2 sourced values across conditions
Tensile strength1,720 to 1,860 MPa1 sourced value
Young's modulus185 to 195 GPa1 sourced value

What is the density of Maraging 250 steel?

Maraging 250 steel has a density of 8 to 8.1 g/cm³. The source and test conditions are listed in the properties table on this page.

What is the yield strength of Maraging 250 steel?

Maraging 250 steel has a yield strength of at least 1,655 MPa. The range covers 2 sourced values across the tempers, forms and test conditions the sources report; room-temperature values are used where a source states a temperature.

What is the tensile strength of Maraging 250 steel?

Maraging 250 steel has a tensile strength of 1,720 to 1,860 MPa. The source and test conditions are listed in the properties table on this page.

What is the Young's modulus of Maraging 250 steel?

Maraging 250 steel has a Young's modulus of 185 to 195 GPa. The source and test conditions are listed in the properties table on this page.

What are the other names and codes for Maraging 250 steel?

Maraging 250 steel is also written as UNS K92890, EN 1.6359, EN name X2NiCoMo18-8-5, BS S162, AMS 6512, ASTM A538. Each code is printed in the source listed beside it in the designations table.

What is Maraging 250 steel used for?

Uses recorded in the sources include Missile and rocket motor cases; Aircraft landing gear components; Aerospace structural and component parts.

Why it exists

Maraging 250 steel (also called VASCOMAX 250 and specified as AMS 6512) is an ultra-high-strength steel. It is supplied in the annealed, descaled condition. The Dynamic Metals die-casting route anneals after rough machining and ages after finish machining. Service Steel Aerospace describes the grade as an 18% nickel, cobalt strengthened steel. Suppliers list it for rocket motor cases, landing gear components, shafts, gears, fasteners and tooling.

Where it's used

Rocket motor cases and missiles

Dynamic Metals lists missile and rocket motor cases among the applications for MARAGING (C) 250. The source is a supplier slide, not a flight record.

Landing gear

Sakysteel lists aircraft landing gear components among its applications for Maraging 250. SSA lists aerospace, structural, component and tooling applications in the same way.

Shafts, gears and fasteners

Dynamic Metals lists high-performance shafting, gears and fasteners. No space flight use was found in the sources we hold.

Recipe

Fe-based alloy with nominal Ni 18.50, Co 7.50, Mo 4.80, Ti 0.40, Al 0.10 (SSA nominal, wt %); reference ranges Ni 17.00 to 19.00, Co 7.00 to 8.50, Mo 4.60 to 5.20, Ti 0.30 to 0.50, Al 0.05 to 0.15 (Dynamic Metals), balance Fe

Maraging 250 is an iron-nickel-cobalt-molybdenum steel. Suppliers supply it in the solution-annealed condition and age it at a low temperature (Sakysteel prints about 480 °C for about 3 to 6 hours). Supplier pages describe it as double vacuum melted by VIM followed by VAR.

What Maraging 250 is made of
IngredientShare of the weightWhat it does
Nickel Ni not stated Main alloying element. The Sakysteel page calls it an 18% nickel, cobalt strengthened steel (C-type).
Cobalt Co not stated Cobalt strengthened steel (SSA wording).
Molybdenum Mo not stated Alloying element listed in both composition tables.
Titanium Ti not stated Alloying element listed in both composition tables.
Aluminium Al not stated Alloying element listed in both composition tables.
Iron Fe not stated Balance of the composition in both sources.

Weight shares are as printed in the sources.

What it can do

Strength

240 ksi

measured

After heat treatment Dynamic Metals gives a minimum yield strength of 240 ksi. Sakysteel gives a minimum reference of 1655 MPa for the aged condition, with a tensile range of 1720 to 1860 MPa.

Machinability before aging

30 to 35 HRC

measured

In the solution-annealed condition the steel is 30 to 35 HRC according to Sakysteel, which is soft enough to machine before it is aged to 48 to 52 HRC.

Density

8.0 to 8.1 g/cm3

measured

The density is printed as an approximate 8.0 to 8.1 g/cm3 (Sakysteel). No other density value was read in a source that states its condition.

How it compares

The sources give Maraging 250 a density of 8.0 to 8.1 g/cm3 (Sakysteel, approximate) and a solution-annealed hardness of 30 to 35 HRC, against 48 to 52 HRC when aged (Sakysteel). The USGS says that titanium alloys can substitute for nickel or nickel-base alloys in corrosive environments, but no source held gives a corrosion rating for Maraging 250, so a like-for-like corrosion comparison cannot be made from this profile.

The same measurements for each material, so you can compare them. Each row names the key condition under the value; the full conditions and methods are in the numbered notes under Technical details.

Benchmarks
MeasurementMaraging 250
Capacity and energy
Charpy V-notch energy, Maraging 250 (minimum after heat treatment)> 15 ft/lbs7
Physical and electrical
Density, Maraging 250 bar8 to 8.1 g/cm³1
Hardness, aged Maraging 250Approximate range printed on a supplier table48 to 52 HRC
Hardness, Maraging 250 (minimum after heat treatment)> 48 Rc6
Hardness, solution-annealed Maraging 250Approximate range printed on a supplier table30 to 35 HRC
Hardness, as-shipped annealed and descaled Maraging 250Range printed on a slide30 to 34 Rc
Hardness, aged Maraging 250 (after 900/925 F for 6 hours)48 to 52 Rc11
Hardness, solution-annealed Maraging 250 (SSA)Range printed on a supplier page30 to 35 Rc
Temperature behavior
Solution treatment temperature, Maraging 250Approximate range printed on a supplier table815 to 830 °C
Aging temperature, Maraging 250 (typical)Typical value printed on a supplier table480 °C9
Aging temperature, Maraging 250 (non-die-casting cycle)Cycle printed on a slide900 F10
Aging temperature, Maraging 250 (SSA cycle)900 to 925 F12
Other measurements
Elastic modulus, Maraging 250Approximate range printed on a supplier table185 to 195 GPa
Tensile strength, aged Maraging 250Approximate range printed on a supplier table1720 to 1860 MPa2
0.2% yield strength, aged Maraging 250 (minimum reference)Minimum reference printed on a supplier table> 1655 MPa3
Yield strength, Maraging 250 (minimum after heat treatment)> 240 ksi4
Elongation, aged Maraging 250Approximate range printed on a supplier table5 to 8 %
Elongation, Maraging 250 (minimum after heat treatment)> 6 %5
Reduction of area, Maraging 250 (minimum after heat treatment)> 50 %8

Why choose it, and why not

Good for

  • Very high strength in a machinable steel, with a yield strength of 240 ksi minimum after heat treatment (Dynamic Metals).
  • Parts that need strength after a low-temperature aging step, such as rocket motor cases and landing gear components (Sakysteel, Dynamic Metals).

Watch out for

  • No corrosion data was found for this grade in any source we hold.
  • Property values depend on bar size, test direction and aging cycle, and the test direction is not stated on any page.
  • The cobalt in the alloy carries its own hazard statements, including 'May cause cancer', from PubChem.

Maraging 250 is a machinable high-strength steel for rocket and landing gear parts, but the corrosion behaviour needs a supplier certificate or a test before use.

Technical details

For scientists and researchers. Everything above comes from the record below: every number with its method, its conditions and its source.

Other names and standards

The same grade under other systems, as datasheets and standards print them. Each code was checked against the page it comes from.

Other names and standards
SystemCodes
UNSK92890
EN1.6359
EN nameX2NiCoMo18-8-5
BSS162
AMS6512
ASTMA538
Trade nameVASCOMAX

Notes

The method, full conditions and any caveat for the numbered rows above.

Notes for the numbered rows
#MeasurementMethodConditionsCaveat
1Density, Maraging 250 barApproximate range printed on a supplier mechanical and heat-treatment tableform bar as printed (no form or temper stated beyond the cited page)temperature room temperaturePrinted as Approx. 8.0-8.1 g/cm3 (Sakysteel). Dynamic Metals prints 0.289 lbs./cu. In. without a stated condition.
2Tensile strength, aged Maraging 250—condition agedorientation not stated on the pagesize results depend on bar size, test orientation, melting route and aging treatment (page text)—
30.2% yield strength, aged Maraging 250 (minimum reference)—condition agedoffset 0.2%basis minimum reference value printed on the page—
4Yield strength, Maraging 250 (minimum after heat treatment)Minimum printed on a slide of mechanical propertiescondition after heat treatment as printed (aging cycle not named)orientation not statedDynamic Metals gives 240 ksi as a minimum; Sakysteel gives 1655 MPa as a minimum reference. The two are consistent in magnitude but use different units and conditions.
5Elongation, Maraging 250 (minimum after heat treatment)Minimum printed on a slide of mechanical propertiescondition after heat treatment as printed (aging cycle not named)—
6Hardness, Maraging 250 (minimum after heat treatment)Minimum printed on a slide of mechanical propertiescondition after heat treatment as printed (aging cycle not named)—
7Charpy V-notch energy, Maraging 250 (minimum after heat treatment)Minimum printed on a slide of mechanical propertiescondition after heat treatment as printed (aging cycle not named)notch V-notch—
8Reduction of area, Maraging 250 (minimum after heat treatment)Minimum printed on a slide of mechanical propertiescondition after heat treatment as printed (aging cycle not named)—
9Aging temperature, Maraging 250 (typical)—step agingduration about 3 to 6 hours as printedcooling air cooled—
10Aging temperature, Maraging 250 (non-die-casting cycle)—step agingtolerance plus or minus 10 F as printedduration 6 hourscooling cool in room air—
11Hardness, aged Maraging 250 (after 900/925 F for 6 hours)Range printed in a heat-treatment table on a supplier pagecondition aged at 900/925 F for 6 hours—
12Aging temperature, Maraging 250 (SSA cycle)Temperature range printed in a heat-treatment table on a supplier pagestep agingduration 6 hours—

Corrosion and compatibility

What happens when it meets other materials and environments.

Corrosion and compatibility
EnvironmentConcernWhat happens
Not stated in any source we hold not rated Corrosion resistance of Maraging 250 was not found in any source we hold, so no corrosion rating is given.1
Corrosion details
#EnvironmentDetailsTest conditions
1 Not stated in any source we hold Three supplier pages and one slide cover mechanical and physical properties, heat treatment and applications. None gives a corrosion test, a corrosion rate or a statement on resistance to a named medium. Titanium alloys can substitute for nickel-base alloys in corrosive environments according to USGS, but that statement concerns other materials. basis absence of any corrosion data in the cited pages

Risks and side effects

Hazards to people, what happens when a cell overheats, and how the material is handled and stored.

For people

No safety data sheet or GHS entry for Maraging 250 itself was found. The entries below are for cobalt metal, a constituent.

Cobalt metal
PubChem's aggregated entry for cobalt metal lists statements including 'May cause cancer', 'Fatal if inhaled' and 'Suspected of causing genetic defects'. These describe the element, not this alloy.
Dust and fume
No exposure limit or dust data for this grade was found in the sources we hold.

If a part fails in service

The sources give no failure test data for this grade.

Aging route
Properties depend on the aging cycle, bar size, test orientation and melting route, according to Sakysteel.

Handling and processing

Die casting route
Dynamic Metals prints an anneal of 1500-1525 F for 1 hour per inch of thickness after rough machining, then aging at 980-1000 F for 6 hours after finish machining.
Annealed state
The as-shipped condition is annealed and descaled, at 30/34 Rc (Dynamic Metals) or 30/35 Rc (SSA).

Test details
The original wording and numbers from the sources, for readers who want them.

Failure risks

Failure risks
FailureTrigger and consequence
Properties depend on the aging cyclemoderate severityAging away from the printed cycle (900 F plus or minus 10 F for 6 hours in the Dynamic Metals non-die-casting route)Sakysteel says results depend on 'bar size, test orientation, melting route, and aging treatment', so a strength value from one cycle cannot be assumed for another.
Test direction not stated on the supplier datalow severityUsing a property value taken from a bar or slide without its test directionDynamic Metals states that the page does not specify test direction (longitudinal or transverse) for any property, so a value may not apply to the orientation a part is loaded in.

Handling and storage

  • Die-casting route, as printed: 'anneal at 1500-1525 F for 1 hour per inch of thickness' after rough machining, then 'age at 980-1000 F for 6 hours' after finish machining.
  • Supplied in the annealed and descaled condition. Sakysteel prints a solution-annealed hardness of 30 to 35 HRC, and Dynamic Metals prints 30/34 Rc as shipped.

Supply and geography

How common the raw materials are and where they come from.

Cobalt (a main alloying element)

Not stated in the sources we hold for this profile.

Top producers (2025)
Congo (Kinshasa) 73%, Indonesia 14%
Critical mineral lists
US: listed, EU: listed
Recycling
USGS: cobalt content of purchased scrap represented 25% of estimated cobalt consumption in 2025.
Substitutes
USGS: depending on the application, substitution for cobalt could result in a loss in product performance or increased cost.

Nickel (main alloying element)

Critical mineral lists
US: listed, EU: listed
Recycling
USGS: nickel recovered from scrap accounted for approximately 60% of apparent consumption in 2025.
Substitutes
USGS: titanium alloys can substitute for nickel or nickel-base alloys in corrosive environments.

Molybdenum (a main alloying element)

Critical mineral lists
US: not listed, EU: not listed
Recycling
USGS: molybdenum may be recycled as much as 30% of apparent supply as part of steel and other scrap.

Titanium sponge (titanium alloying element)

Critical mineral lists
US: listed, EU: listed
Recycling
USGS: limited responses to voluntary surveys mean the consumption data for titanium scrap metal are incomplete.
Substitutes
USGS: few materials possess titanium metal's strength-to-weight ratio and corrosion resistance.

Updated