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.
Evidence level
2 of 5
Lab-measured
- 0Predicted only. No one has made it, or no measurement exists.
- 1Calculated. Only calculated or predicted values from sources.
- 2Lab-measured. Measured properties with their conditions stated.
- 3Space-relevant tests. Measured in conditions relevant to space, such as vacuum or atomic oxygen.
- 4Ground-qualified. Qualified for an application on the ground.
- 5Flown or field-proven. Flight or field results exist.
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
| Property | Value | Basis |
|---|---|---|
| Density | 8 to 8.1 g/cm³ | 1 sourced value |
| Yield strength | at least 1,655 MPa | 2 sourced values across conditions |
| Tensile strength | 1,720 to 1,860 MPa | 1 sourced value |
| Young's modulus | 185 to 195 GPa | 1 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.
| Ingredient | Share of the weight | What 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.
| Measurement | Maraging 250 |
|---|---|
| Capacity and energy | |
| Charpy V-notch energy, Maraging 250 (minimum after heat treatment) | > 15 ft/lbs7 |
| Physical and electrical | |
| Density, Maraging 250 bar | 8 to 8.1 g/cm³1 |
| Hardness, aged Maraging 250Approximate range printed on a supplier table | 48 to 52 HRC |
| Hardness, Maraging 250 (minimum after heat treatment) | > 48 Rc6 |
| Hardness, solution-annealed Maraging 250Approximate range printed on a supplier table | 30 to 35 HRC |
| Hardness, as-shipped annealed and descaled Maraging 250Range printed on a slide | 30 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 page | 30 to 35 Rc |
| Temperature behavior | |
| Solution treatment temperature, Maraging 250Approximate range printed on a supplier table | 815 to 830 °C |
| Aging temperature, Maraging 250 (typical)Typical value printed on a supplier table | 480 °C9 |
| Aging temperature, Maraging 250 (non-die-casting cycle)Cycle printed on a slide | 900 F10 |
| Aging temperature, Maraging 250 (SSA cycle) | 900 to 925 F12 |
| Other measurements | |
| Elastic modulus, Maraging 250Approximate range printed on a supplier table | 185 to 195 GPa |
| Tensile strength, aged Maraging 250Approximate range printed on a supplier table | 1720 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 table | 5 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.
| System | Codes |
|---|---|
| UNS | K92890 |
| EN | 1.6359 |
| EN name | X2NiCoMo18-8-5 |
| BS | S162 |
| AMS | 6512 |
| ASTM | A538 |
| Trade name | VASCOMAX |
Notes
The method, full conditions and any caveat for the numbered rows above.
| # | Measurement | Method | Conditions | Caveat |
|---|---|---|---|---|
| 1 | Density, Maraging 250 bar | Approximate range printed on a supplier mechanical and heat-treatment table | form bar as printed (no form or temper stated beyond the cited page)temperature room temperature | Printed as Approx. 8.0-8.1 g/cm3 (Sakysteel). Dynamic Metals prints 0.289 lbs./cu. In. without a stated condition. |
| 2 | Tensile 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) | — |
| 3 | 0.2% yield strength, aged Maraging 250 (minimum reference) | — | condition agedoffset 0.2%basis minimum reference value printed on the page | — |
| 4 | Yield strength, Maraging 250 (minimum after heat treatment) | Minimum printed on a slide of mechanical properties | condition after heat treatment as printed (aging cycle not named)orientation not stated | Dynamic 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. |
| 5 | Elongation, Maraging 250 (minimum after heat treatment) | Minimum printed on a slide of mechanical properties | condition after heat treatment as printed (aging cycle not named) | — |
| 6 | Hardness, Maraging 250 (minimum after heat treatment) | Minimum printed on a slide of mechanical properties | condition after heat treatment as printed (aging cycle not named) | — |
| 7 | Charpy V-notch energy, Maraging 250 (minimum after heat treatment) | Minimum printed on a slide of mechanical properties | condition after heat treatment as printed (aging cycle not named)notch V-notch | — |
| 8 | Reduction of area, Maraging 250 (minimum after heat treatment) | Minimum printed on a slide of mechanical properties | condition after heat treatment as printed (aging cycle not named) | — |
| 9 | Aging temperature, Maraging 250 (typical) | — | step agingduration about 3 to 6 hours as printedcooling air cooled | — |
| 10 | Aging temperature, Maraging 250 (non-die-casting cycle) | — | step agingtolerance plus or minus 10 F as printedduration 6 hourscooling cool in room air | — |
| 11 | Hardness, aged Maraging 250 (after 900/925 F for 6 hours) | Range printed in a heat-treatment table on a supplier page | condition aged at 900/925 F for 6 hours | — |
| 12 | Aging temperature, Maraging 250 (SSA cycle) | Temperature range printed in a heat-treatment table on a supplier page | step agingduration 6 hours | — |
Corrosion and compatibility
What happens when it meets other materials and environments.
| Environment | Concern | What 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 |
| # | Environment | Details | Test 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 | Trigger and consequence |
|---|---|
| Properties depend on the aging cyclemoderate severity | Aging 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 severity | Using 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.
Documents
Datasheets, safety data sheets, papers and standards you can open.
| Document | Type | Year |
|---|---|---|
| Service Steel Aerospace: Maraging 250 (AMS 6512) product and mechanical properties page | datasheet | 2026 |
| Sakysteel: Maraging 250 steel round bar product page | datasheet | 2026 |
| Dynamic Metals International: MARAGING (C) 250 slide (SlideShare) | datasheet | 2026 |
| USGS Mineral Commodity Summaries 2026: Cobalt | report | 2026 |
| USGS Mineral Commodity Summaries 2026: Nickel | report | 2026 |
| USGS Mineral Commodity Summaries 2026: Molybdenum | report | 2026 |
| USGS Mineral Commodity Summaries 2026: Titanium | report | 2026 |
| PubChem: Cobalt (CID 104730), GHS classification | database | 2026 |
Full record
The complete spore, as stored. Free to reuse under CC-BY-4.0. Images keep the licence shown with each one.
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spore: profile
id: maraging-steel-250
spore_version: 0.2
family: maraging-steels
name: Maraging 250 steel
abbreviation: Maraging 250
role: ultra-high-strength structural steel
category: metals
type: steels-and-stainless
summary: |
Maraging 250 steel is an 18% nickel, cobalt-strengthened steel (C-type) that is aged at a low temperature to reach its strength. Aged at about 480 °C for about 3 to 6 hours (Sakysteel), it has a tensile strength of 1720 to 1860 MPa and a density of 8.0 to 8.1 g/cm3 (Sakysteel, approximate values). Its solution-annealed hardness is 30 to 35 HRC (Sakysteel), so it can be machined before it is aged. Corrosion resistance was not found in any source we hold.
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
identity:
formula: 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
source: dmi-maraging-250
where: Chemical Composition table (Dynamic Metals slide, wt %); SSA Chemical Composition table (Nominal %)
designations:
- system: UNS
code: K92890
source: sakysteel-maraging-250
where: Product table, UNS line
- system: AMS
code: '6512'
source: ssa-maraging-250
where: Page title and product description (AMS 6512 primary bar and forging-stock specification)
- system: EN
code: '1.6359'
source: sakysteel-maraging-250
where: EN/European reference line (W.Nr. 1.6359)
- system: EN name
code: X2NiCoMo18-8-5
source: sakysteel-maraging-250
where: Product parameters table, X2NiCoMo18-8-5 reference
- system: BS
code: S162
source: sakysteel-maraging-250
where: British reference line (BS S162 / DTD 5212)
- system: ASTM
code: A538
note: printed as ASTM A 538; listed on the Standards line
source: dmi-maraging-250
where: Standards line
- system: Trade name
code: VASCOMAX
note: printed as VASCOMAX® 250 on the SSA page (the 250 is the grade number)
source: ssa-maraging-250
where: Product name line
tags:
environments: []
stresses: []
applications:
- structures
- propulsion-and-tanks
- mechanisms
properties:
- benchmark: density
label: Density, Maraging 250 bar
value: 8
value_high: 8.1
bound: range
unit: g/cm3
scope: material
conditions:
form: bar as printed (no form or temper stated beyond the cited page)
temperature: room temperature
method: Approximate range printed on a supplier mechanical and heat-treatment table
status: ground
note: Printed as Approx. 8.0-8.1 g/cm3 (Sakysteel). Dynamic Metals prints 0.289 lbs./cu. In. without a stated condition.
source: sakysteel-maraging-250
where: Mechanical and Heat-Treatment Properties table, Density row
- benchmark: elastic_modulus
label: Elastic modulus, Maraging 250
value: 185
value_high: 195
bound: range
unit: GPa
scope: material
conditions:
temperature: room temperature
condition: as printed for the aged condition
method: Approximate range printed on a supplier table
status: ground
source: sakysteel-maraging-250
where: Mechanical and Heat-Treatment Properties table, Elastic Modulus row
- benchmark: ultimate_tensile_strength
label: Tensile strength, aged Maraging 250
value: 1720
value_high: 1860
bound: range
unit: MPa
scope: material
conditions:
condition: aged
orientation: not stated on the page
size: results depend on bar size, test orientation, melting route and aging treatment (page text)
method: Approximate range printed on a supplier table
status: ground
source: sakysteel-maraging-250
where: Mechanical and Heat-Treatment Properties table, Tensile Strength row
- benchmark: yield_strength
label: 0.2% yield strength, aged Maraging 250 (minimum reference)
value: 1655
bound: lower
unit: MPa
scope: material
conditions:
condition: aged
offset: 0.2%
basis: minimum reference value printed on the page
method: Minimum reference printed on a supplier table
status: ground
source: sakysteel-maraging-250
where: Mechanical and Heat-Treatment Properties table, 0.2% Yield Strength row
- benchmark: yield_strength
label: Yield strength, Maraging 250 (minimum after heat treatment)
value: 240
bound: lower
unit: ksi
scope: material
conditions:
condition: after heat treatment as printed (aging cycle not named)
orientation: not stated
method: Minimum printed on a slide of mechanical properties
status: ground
note: Dynamic 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.
source: dmi-maraging-250
where: Mechanical Properties (Minimum, After Heat Treatment) table, Yield Strength row
- benchmark: elongation
label: Elongation, aged Maraging 250
value: 5
value_high: 8
bound: range
unit: '%'
scope: material
conditions:
condition: aged
size: size dependent, as printed
method: Approximate range printed on a supplier table
status: ground
source: sakysteel-maraging-250
where: Mechanical and Heat-Treatment Properties table, Elongation row
- benchmark: elongation
label: Elongation, Maraging 250 (minimum after heat treatment)
value: 6
bound: lower
unit: '%'
scope: material
conditions:
condition: after heat treatment as printed (aging cycle not named)
method: Minimum printed on a slide of mechanical properties
status: ground
source: dmi-maraging-250
where: Mechanical Properties (Minimum, After Heat Treatment) table, Elongation row
- benchmark: hardness_rockwell_c
label: Hardness, aged Maraging 250
value: 48
value_high: 52
bound: range
unit: HRC
scope: material
conditions:
condition: aged
method: Approximate range printed on a supplier table
status: ground
source: sakysteel-maraging-250
where: Mechanical and Heat-Treatment Properties table, Hardness row
- benchmark: hardness_rockwell_c
label: Hardness, Maraging 250 (minimum after heat treatment)
value: 48
bound: lower
unit: Rc
scope: material
conditions:
condition: after heat treatment as printed (aging cycle not named)
method: Minimum printed on a slide of mechanical properties
status: ground
source: dmi-maraging-250
where: Mechanical Properties (Minimum, After Heat Treatment) table, Hardness row
- benchmark: hardness_rockwell_c
label: Hardness, solution-annealed Maraging 250
value: 30
value_high: 35
bound: range
unit: HRC
scope: material
conditions:
condition: solution annealed
method: Approximate range printed on a supplier table
status: ground
source: sakysteel-maraging-250
where: Mechanical and Heat-Treatment Properties table, Annealed Hardness row
- benchmark: hardness_rockwell_c
label: Hardness, as-shipped annealed and descaled Maraging 250
value: 30
value_high: 34
bound: range
unit: Rc
scope: material
conditions:
condition: annealed and descaled, as shipped
method: Range printed on a slide
status: ground
source: dmi-maraging-250
where: As-shipped condition line
- benchmark: charpy_impact_energy
label: Charpy V-notch energy, Maraging 250 (minimum after heat treatment)
value: 15
bound: lower
unit: ft/lbs
scope: material
conditions:
condition: after heat treatment as printed (aging cycle not named)
notch: V-notch
method: Minimum printed on a slide of mechanical properties
status: ground
source: dmi-maraging-250
where: Mechanical Properties (Minimum, After Heat Treatment) table, Charpy V-notch row
- benchmark: reduction_of_area
label: Reduction of area, Maraging 250 (minimum after heat treatment)
value: 50
bound: lower
unit: '%'
scope: material
conditions:
condition: after heat treatment as printed (aging cycle not named)
method: Minimum printed on a slide of mechanical properties
status: ground
source: dmi-maraging-250
where: Mechanical Properties (Minimum, After Heat Treatment) table, Reduction of Area row
- benchmark: solution_treatment_temperature
label: Solution treatment temperature, Maraging 250
value: 815
value_high: 830
bound: range
unit: °C
scope: material
conditions:
step: solution treatment
cooling: air cooled
method: Approximate range printed on a supplier table
status: ground
source: sakysteel-maraging-250
where: Mechanical and Heat-Treatment Properties table, Solution Treatment row
- benchmark: aging_temperature
label: Aging temperature, Maraging 250 (typical)
value: 480
unit: °C
scope: material
conditions:
step: aging
duration: about 3 to 6 hours as printed
cooling: air cooled
method: Typical value printed on a supplier table
status: ground
source: sakysteel-maraging-250
where: Mechanical and Heat-Treatment Properties table, Typical Aging row
- benchmark: aging_temperature
label: Aging temperature, Maraging 250 (non-die-casting cycle)
value: 900
unit: F
scope: material
conditions:
step: aging
tolerance: plus or minus 10 F as printed
duration: 6 hours
cooling: cool in room air
method: Cycle printed on a slide
status: ground
source: dmi-maraging-250
where: Heat Treatment (Slide 1), non-die-casting applications
- benchmark: hardness_rockwell_c
label: Hardness, aged Maraging 250 (after 900/925 F for 6 hours)
value: 48
value_high: 52
bound: range
unit: Rc
scope: material
conditions:
condition: aged at 900/925 F for 6 hours
method: Range printed in a heat-treatment table on a supplier page
status: ground
source: ssa-maraging-250
where: Heat Treatment / Aging table, Resulting Hardness row
- benchmark: hardness_rockwell_c
label: Hardness, solution-annealed Maraging 250 (SSA)
value: 30
value_high: 35
bound: range
unit: Rc
scope: material
conditions:
condition: solution annealed
method: Range printed on a supplier page
status: ground
source: ssa-maraging-250
where: Heat Treatment / Aging section, solution annealed condition line
- benchmark: aging_temperature
label: Aging temperature, Maraging 250 (SSA cycle)
value: 900
value_high: 925
bound: range
unit: F
scope: material
conditions:
step: aging
duration: 6 hours
method: Temperature range printed in a heat-treatment table on a supplier page
status: ground
source: ssa-maraging-250
where: Heat Treatment / Aging table, Temperature row
corrosion:
- environment: Not stated in any source we hold
headline: Corrosion resistance of Maraging 250 was not found in any source we hold, so no corrosion rating is given.
effect: 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.
rating: unknown
conditions:
basis: absence of any corrosion data in the cited pages
source: ssa-maraging-250
where: Whole page checked; no corrosion section
risks:
hazards:
- text: The alloy itself has no GHS entry we could read. The hazard entries below are for cobalt metal, a constituent of the alloy, and do not measure this grade. PubChem's aggregated cobalt entry lists 'Harmful if swallowed', 'May cause an allergic skin reaction', 'Causes serious eye irritation', 'Fatal if inhaled', 'May cause allergy or asthma symptoms or breathing difficulties if inhaled', 'Suspected of causing genetic defects', 'May cause cancer' and 'May damage fertility; Suspected of damaging the unborn child'.
ghs:
- H302
- H317
- H319
- H330
- H334
- H341
- H350
- H360Fd
source: pubchem-cobalt
where: GHS Classification section, aggregated entry, CID 104730 (cobalt)
- text: The same PubChem entry lists 'Very toxic to aquatic life' and 'Toxic to aquatic life with long lasting effects' for cobalt metal, with a signal word of Danger on the aggregated entry.
ghs:
- H400
- H410
- H411
- H413
source: pubchem-cobalt
where: GHS Classification section, aggregated entry, CID 104730 (cobalt)
failure_risks:
- mode: Properties depend on the aging cycle
trigger: Aging away from the printed cycle (900 F plus or minus 10 F for 6 hours in the Dynamic Metals non-die-casting route)
consequence: 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.
severity: moderate
source: sakysteel-maraging-250
where: Chemical and heat-treatment notes; Mechanical and Heat-Treatment Properties table
- mode: Test direction not stated on the supplier data
trigger: Using a property value taken from a bar or slide without its test direction
consequence: Dynamic 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.
severity: low
source: dmi-maraging-250
where: Mechanical Properties (Minimum, After Heat Treatment) table
handling:
- text: '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.'
source: dmi-maraging-250
where: Heat Treatment (Slide 1), die-casting applications
- text: 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.
source: sakysteel-maraging-250
where: Annealed Hardness row; Dynamic Metals As-shipped condition line
uses:
- application: propulsion-and-tanks
device: Missile and rocket motor cases
example: Dynamic Metals lists missile and rocket motor cases among the applications for MARAGING (C) 250.
source: dmi-maraging-250
where: Listed Applications
- application: structures
device: Aircraft landing gear components
example: Sakysteel lists aircraft landing gear components among the applications for Maraging 250.
source: sakysteel-maraging-250
where: Listed Applications
- application: structures
device: Aerospace structural and component parts
example: SSA lists aerospace, structural, component and tooling applications for Maraging 250, with critical parts among them.
source: ssa-maraging-250
where: Applications (as listed)
- application: mechanisms
device: High-performance shafting, gears and fasteners
example: Dynamic Metals lists high-performance shafting, gears and fasteners among its applications for MARAGING (C) 250.
source: dmi-maraging-250
where: Listed Applications
supply:
- subject: Cobalt (a main alloying element)
abundance: Not stated in the sources we hold for this profile.
producers:
- country: Congo (Kinshasa)
share_percent: 73
year: 2025
- country: Indonesia
share_percent: 14
year: 2025
critical_lists:
- list: USGS 2025 List of Critical Minerals (page lists cobalt)
listed: true
- list: European Commission critical raw materials page (lists Cobalt)
listed: true
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.'
source: usgs-mcs2026-cobalt
where: Events, Trends, and Issues (Congo and Indonesia shares, printed); World Mine Production table (world total 310,000 metric tons in 2025, cobalt content); Recycling; Substitutes
- subject: Nickel (main alloying element)
producers: []
critical_lists:
- list: USGS 2025 List of Critical Minerals (page lists nickel)
listed: true
- list: European Commission critical raw materials page (nickel included as a strategic raw material)
listed: true
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.'
source: usgs-mcs2026-nickel
where: World Mine Production and Reserves table (world total 3,900,000 metric tons in 2025, nickel content); Events (3.9 million tons in 2025); Recycling; Substitutes
- subject: Molybdenum (a main alloying element)
producers: []
critical_lists:
- list: USGS 2025 List of Critical Minerals (molybdenum not listed)
listed: false
- list: European Commission critical raw materials page (molybdenum not listed)
listed: false
recycling: 'USGS: molybdenum may be recycled as much as 30% of apparent supply as part of steel and other scrap.'
substitutes: []
source: usgs-mcs2026-molybdenum
where: Recycling paragraph; Events (China, Chile, the United States, Peru and Mexico accounted for 90% of total global production); World Mine Production table (world total 260,000 metric tons in 2025, molybdenum content)
- subject: Titanium sponge (titanium alloying element)
producers: []
critical_lists:
- list: USGS 2025 List of Critical Minerals (page lists titanium, used in metal alloys)
listed: true
- list: European Commission critical raw materials page (titanium metal listed)
listed: true
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.'
source: usgs-mcs2026-titanium
where: World Sponge Metal Production table (world total 370,000 metric tons in 2025; China 260,000); Recycling; Substitutes
media: []
documents:
- title: 'Service Steel Aerospace: Maraging 250 (AMS 6512) product and mechanical properties page'
type: datasheet
url: https://ssa-corp.com/he/maraging-250-AMS-6512.php
year: 2026
- title: 'Sakysteel: Maraging 250 steel round bar product page'
type: datasheet
url: https://m.sakysteel.com/maraging-250-steel-round-bar.html
year: 2026
- title: 'Dynamic Metals International: MARAGING (C) 250 slide (SlideShare)'
type: datasheet
url: https://www.slideshare.net/slideshow/maraging-250-spec/48297132
year: 2026
- title: 'USGS Mineral Commodity Summaries 2026: Cobalt'
type: report
url: https://pubs.usgs.gov/periodicals/mcs2026/mcs2026-cobalt.pdf
year: 2026
- title: 'USGS Mineral Commodity Summaries 2026: Nickel'
type: report
url: https://pubs.usgs.gov/periodicals/mcs2026/mcs2026-nickel.pdf
year: 2026
- title: 'USGS Mineral Commodity Summaries 2026: Molybdenum'
type: report
url: https://pubs.usgs.gov/periodicals/mcs2026/mcs2026-molybdenum.pdf
year: 2026
- title: 'USGS Mineral Commodity Summaries 2026: Titanium'
type: report
url: https://pubs.usgs.gov/periodicals/mcs2026/mcs2026-titanium.pdf
year: 2026
- title: 'PubChem: Cobalt (CID 104730), GHS classification'
type: database
url: https://pubchem.ncbi.nlm.nih.gov/compound/104730
year: 2026
gaps:
- 'Corrosion resistance of Maraging 250 in any medium: not found in any source we hold. The corrosion entry is rated unknown on purpose.'
- 'Fracture toughness: Dynamic Metals prints ''75 KIC'' with no unit, so the value was left out.'
- 'Coefficient of thermal expansion: the pages print ''5.6 x 10-6'' with the exponent in a non-standard form, so the value was left out. Dynamic Metals gives 5.6 x 10 -6 in/in. F for 70 to 900 F.'
- 'Modulus: SSA prints ''27.0 x 10-6 psi'', which looks like a typo for 10^6 and is not used; the Sakysteel range in GPa is recorded instead.'
- 'Test direction (longitudinal or transverse) for any property: not stated on any page.'
- No SDS or safety page for Maraging 250 itself was found. Hazard entries are for cobalt metal, a constituent.
- Nickel, molybdenum and titanium producer shares by country were not printed in the pages used, so supply rows give the world totals, not shares.
- UNS and EN designations were checked against the printed pages; the 18Ni(250) name is not printed in any source, so only 18Ni250 is used, as a grade name on the Sakysteel page.
- 'Seven Dynamic Metals values and its ASTM A 538 designation could not be machine-checked: the SlideShare page returned no text to verify-values. They were read in this run with WebFetch and are flagged for a manual check.'
- Peer-reviewed or open-access papers on Maraging 250 were not reached in this run; the properties rest on supplier pages and one slide.
sources:
ssa-maraging-250:
title: Maraging 250 (AMS 6512), Service Steel Aerospace product page
id: SSA page, maraging-250-AMS-6512
url: https://ssa-corp.com/he/maraging-250-AMS-6512.php
year: 2026
kind: web
license: supplier page, cited not reproduced
sakysteel-maraging-250:
title: Maraging 250 steel round bar, Sakysteel product page
id: Sakysteel product page
url: https://m.sakysteel.com/maraging-250-steel-round-bar.html
year: 2026
kind: web
license: supplier page, cited not reproduced
dmi-maraging-250:
title: MARAGING (C) 250, Dynamic Metals International slide (SlideShare)
id: SlideShare 48297132
url: https://www.slideshare.net/slideshow/maraging-250-spec/48297132
year: 2026
kind: datasheet
license: slide, cited not reproduced
usgs-mcs2026-cobalt:
title: Mineral Commodity Summaries 2026, Cobalt
id: USGS MCS 2026
url: https://pubs.usgs.gov/periodicals/mcs2026/mcs2026-cobalt.pdf
year: 2026
kind: report
license: public domain (USGS)
usgs-mcs2026-nickel:
title: Mineral Commodity Summaries 2026, Nickel
id: USGS MCS 2026
url: https://pubs.usgs.gov/periodicals/mcs2026/mcs2026-nickel.pdf
year: 2026
kind: report
license: public domain (USGS)
usgs-mcs2026-molybdenum:
title: Mineral Commodity Summaries 2026, Molybdenum
id: USGS MCS 2026
url: https://pubs.usgs.gov/periodicals/mcs2026/mcs2026-molybdenum.pdf
year: 2026
kind: report
license: public domain (USGS)
usgs-mcs2026-titanium:
title: Mineral Commodity Summaries 2026, Titanium
id: USGS MCS 2026
url: https://pubs.usgs.gov/periodicals/mcs2026/mcs2026-titanium.pdf
year: 2026
kind: report
license: public domain (USGS)
pubchem-cobalt:
title: PubChem compound record, Cobalt (CID 104730), GHS classification
id: CID 104730
url: https://pubchem.ncbi.nlm.nih.gov/compound/104730
year: 2026
kind: database
license: public domain (NCBI)
usgs-crit2025:
title: About the 2025 List of Critical Minerals (USGS)
id: USGS final 2025 list
url: https://www.usgs.gov/programs/mineral-resources-program/science/about-2025-list-critical-minerals
year: 2025
kind: web
license: public domain (USGS)
ec-crm:
title: Critical raw materials (European Commission page, 34 materials)
id: European Commission CRM page
url: https://single-market-economy.ec.europa.eu/sectors/raw-materials/areas-specific-interest/critical-raw-materials_en
year: 2024
kind: web
license: European Commission web page
license: CC-BY-4.0
updated: '2026-11-01'
review:
status: draft
method: assistant
checked_values: 19
unreachable: 0
caveats: 2
note: Written by an AI assistant on 2026-11-01 from pages fetched in that run. Supplier values are approximate or minimum values as printed; no test-certificate values were available.
story:
recipe:
line: 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.
parts:
- name: Nickel
symbol: Ni
share: 18.50 nominal (SSA); 17.00 to 19.00 (Dynamic Metals), wt %
role: Main alloying element. The Sakysteel page calls it an 18% nickel, cobalt strengthened steel (C-type).
- name: Cobalt
symbol: Co
share: 7.50 nominal (SSA); 7.00 to 8.50 (Dynamic Metals), wt %
role: Cobalt strengthened steel (SSA wording).
- name: Molybdenum
symbol: Mo
share: 4.80 nominal (SSA); 4.60 to 5.20 (Dynamic Metals), wt %
role: Alloying element listed in both composition tables.
- name: Titanium
symbol: Ti
share: 0.40 nominal (SSA); 0.30 to 0.50 (Dynamic Metals), wt %
role: Alloying element listed in both composition tables.
- name: Aluminium
symbol: Al
share: 0.10 nominal (SSA); 0.05 to 0.15 (Dynamic Metals), wt %
role: Alloying element listed in both composition tables.
- name: Iron
symbol: Fe
share: balance
role: Balance of the composition in both sources.
risk_groups:
- title: For people
level: 0
verdict: No alloy hazard entry found
lead: No safety data sheet or GHS entry for Maraging 250 itself was found. The entries below are for cobalt metal, a constituent.
points:
- label: Cobalt metal
line: 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.
- label: Dust and fume
line: No exposure limit or dust data for this grade was found in the sources we hold.
- title: If a part fails in service
lead: The sources give no failure test data for this grade.
points:
- label: Aging route
line: Properties depend on the aging cycle, bar size, test orientation and melting route, according to Sakysteel.
- title: Handling and processing
points:
- label: Die casting route
line: 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.
- label: Annealed state
line: The as-shipped condition is annealed and descaled, at 30/34 Rc (Dynamic Metals) or 30/35 Rc (SSA).
why: 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.
uses:
- where: Rocket motor cases and missiles
line: 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.
- where: Landing gear
line: Sakysteel lists aircraft landing gear components among its applications for Maraging 250. SSA lists aerospace, structural, component and tooling applications in the same way.
- where: Shafts, gears and fasteners
line: Dynamic Metals lists high-performance shafting, gears and fasteners. No space flight use was found in the sources we hold.
can_do:
- label: Strength
benchmark: yield_strength
value: 240 ksi
line: 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.
- label: Machinability before aging
benchmark: hardness_rockwell_c
value: 30 to 35 HRC
line: 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.
- label: Density
benchmark: density
value: 8.0 to 8.1 g/cm3
line: 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.
compare: 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.
compare_rows:
- label: Density
benchmark: density
- label: Tensile strength
benchmark: ultimate_tensile_strength
- label: Yield strength
benchmark: yield_strength
handling:
- Anneal before final machining, using the printed Dynamic Metals die-casting route, or follow the supplier's own cycle.
- The alloy is supplied annealed and descaled. Check the aging cycle against the mill certificate for the bar size.
- No hazard data sheet for the alloy was found, and no dust exposure limit for this grade was found in the sources we hold.
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:
- 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.
verdict: 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.
References
Every number above carries a reference number. Click one to see the source and where in it the value comes from.
| # | Source | Type | Year | Used for |
|---|---|---|---|---|
| Maraging 250 (AMS 6512), Service Steel Aerospace product page | web | 2026 | 5 values | |
| Maraging 250 steel round bar, Sakysteel product page | web | 2026 | 12 values | |
| MARAGING (C) 250, Dynamic Metals International slide (SlideShare) | datasheet | 2026 | 12 values | |
| Mineral Commodity Summaries 2026, Cobalt | report | 2026 | 1 value | |
| Mineral Commodity Summaries 2026, Nickel | report | 2026 | 1 value | |
| Mineral Commodity Summaries 2026, Molybdenum | report | 2026 | 1 value | |
| Mineral Commodity Summaries 2026, Titanium | report | 2026 | 1 value | |
| PubChem compound record, Cobalt (CID 104730), GHS classification | database | 2026 | 2 values | |
| About the 2025 List of Critical Minerals (USGS) | web | 2025 | 0 values | |
| Critical raw materials (European Commission page, 34 materials) | web | 2024 | 0 values |
Updated