Maraging steels (a portmanteau of "martensitic" and "aging") are steels that possess superior strength and toughness without losing ductility. Aging refers to the extended heat-treatment process. These steels are a special class of very-low-carbon ultra-high-strength steels that derive their strength from precipitation of intermetallic compounds rather than from carbon. The principal alloying metal is 15 to 25 wt% nickel. Secondary alloying metals, which include cobalt, molybdenum and titanium, are added to produce intermetallic precipitates. The intent was to induce age-hardening with the aforementioned intermetallics in an iron-nickel martensitic matrix, and it was discovered that Co and Mo complement each other very well. Commercial production started in December 1960. A rise in the price of Co in the late 1970s led to cobalt-free maraging steels.
The common, non-stainless grades contain 17–19 wt% Ni, 8–12 wt% Co, 3–5 wt% Mo and 0.2–1.6 wt% Ti. Addition of chromium produces corrosion-resistant stainless grades. This also indirectly increases hardenability as they require less Ni; high-Cr, high-Ni steels are generally austenitic and unable to become martensite when heat treated, while lower-Ni steels can.
Alternative variants of Ni-reduced maraging steels are based on alloys of Fe and Mn plus minor additions of Al, Ni and Ti with compositions between Fe-9wt% Mn to Fe-15wt% Mn qualify used. The manganese has an effect similar to nickel, i.e. it stabilizes the austenite phase. Hence, depending on their manganese content, Fe-Mn maraging steels can be fully martensitic after quenching them from the high temperature austenite phase or they can contain retained austenite. The latter effect enables the design of maraging-transformation-induced-plasticity (TRIP) steels.
Properties
Due to the low carbon content (less than 0.03%) maraging steels have good machinability. Prior to aging, they may also be cold rolled to as much as 90% without cracking. Maraging steels offer good weldability, but must be aged afterward to restore the original properties to the heat affected zone. The higher grades have more cobalt and titanium in the alloy; the compositions below are taken from table 1 of MIL-S-46850D. As of July 1, 2024, that standard was cancelled by the U.S. Military and replaced with a number of SAE AMS specifications, which now govern each grade in a separate specification, as enumerated below.
{| class="wikitable" style="text-align:center;"
|+ Maraging steel compositions, by grade
! scope="col"| Element
! scope="col"| Grade 200
! scope="col"| Grade 250
! scope="col"| Grade 300
! scope="col"| Grade 350
|-
! scope="row"| Iron
|balance||balance||balance||balance
|-
! scope="row"| Nickel
|17.0–19.0||17.0–19.0||18.0–19.0||18.0–19.0
|-
! scope="row"| Cobalt
|8.0–9.0||7.0–8.5||8.5–9.5||11.5–12.5
|-
! scope="row"| Molybdenum
|3.0–3.5||4.6–5.2||4.6–5.2||4.6–5.2
|-
! scope="row"| Titanium
|0.15–0.25||0.3–0.5||0.5–0.8||1.3–1.6
|-
! scope="row"| Aluminium
|0.05–0.15||0.05–0.15||0.05–0.15||0.05–0.15
|-
! scope="row"| Tensile strength, MPa (ksi)
|||||||
|-
! scope="row"| SAE AMS Specification
|AMS6511C||AMS6512J||AMS6514K||AMS6515C
|}
This family is known as the 18Ni maraging steels, from its nickel percentage. There is also a family of cobalt-free maraging steels which are cheaper but not quite as strong; one example is Fe-18.9Ni-4.1Mo-1.9Ti. There has been Russian and Japanese research in Fe-Ni-Mn maraging alloys.
- Laser Powder Bed Fusion (LPBF): Laser Powder Bed Fusion is an additive manufacturing technique used to create components of intricate geometries using a powder metal which is fused together layer by layer using localized high power-density heat source such as a laser. The materials can be tailored to have specific mechanical properties by optimizing the process parameters associated with LPBF. It has been observed that processing parameters such as laser scanning speed, power and the scanning space can have significant effects on the mechanical properties of 300 maraging steel such as tensile strength, microhardness, and impact toughness. Along with the processing parameters, the type of heat treatment subjected to LPBF steels also play an important role. It is observed that processing parameters which have a higher magnitude reduce the relative density of the sample due to rapid vaporization or creation of voids and pores. It is also observed that the microhardness and strength of the steel decreases after solution treatment due to austenite reversion and disappearance of cellular microstructure. On the other hand, aging treatment after solution treatment increases the microhardness and tensile strength of steel which is attributed to formation of precipitates such as Ni<sub>3</sub>Mo, Ni<sub>3</sub>Ti, Fe<sub>2</sub>Mo. The impact toughness increases after solution treatment but decreases after aging treatment, which can be attributed to the underlying microstructure consisting of tiny precipitates acting as regions of stress concentrators for crack formation. Formation of nanoscale precipitates of intermetallic compounds after aging process lead to marked increase in yield and ultimate tensile strength but substantial reduction in ductility of the material. This change in macroscopic behavior of the material can be linked to the evolution of microstructure from dimple to quasi-cleavage fracture morphology. Aging followed by solution treatment of selective laser melted steels also reduces the amount of retained austenite in the martensitic matrix and lead to change in the grain orientation. Aging can reduce the plastic anisotropy to some extent, but directionality of properties is largely influenced by its fabrication history.
- Severe plastic deformation: It leads to increase in dislocation density in the materials which in turn assists in the ease of formation of intermetallic precipitates due to availability of faster diffusion pathways through the dislocation cores. It has been observed that plastic deformation before aging leads to reduced peak aging time and increase in peak hardness. Precipitate morphology in severely plastically deformed steel changes and becomes plate-like when overaged which is attributed to higher dislocation density. This in turn leads to significant reduction in ductility and increase in strength of the material. Along with morphology, the orientation of precipitates also play an important role in micromechanism of deformation as they induce anisotropy to the mechanical properties.
Uses
Maraging steel's strength and malleability in the pre-aged stage allows it to be formed into thinner rocket and missile skins than other steels, reducing weight for a given strength. Maraging steels have very stable properties and, even after overaging due to excessive temperature, only soften slightly. These alloys retain their properties at mildly elevated operating temperatures and have maximum service temperatures of over . They are suitable for engine components, such as crankshafts and gears, and the firing pins of automatic weapons that cycle from hot to cool repeatedly while under substantial load. Their uniform expansion and easy machinability before aging make maraging steel useful in high-wear components of assembly lines and dies. Other ultra-high-strength steels, such as AerMet alloys, are not as machinable because of their carbide content.
In the sport of fencing, blades used in competitions run under the auspices of the Fédération Internationale d'Escrime are usually made with maraging steel. Maraging blades are superior for foil and épée because crack propagation in maraging steel is 10 times slower than in carbon steel, resulting in less frequent breaking of the blade and fewer injuries. Stainless maraging steel is used in bicycle frames (e.g. Reynolds 953 introduced in 2013) and golf club heads. It is also used in surgical components and hypodermic syringes, but is not suitable for scalpel blades because the lack of carbon prevents it from holding a good cutting edge.
Maraging steel is used in oil and gas sector as downhole tools and components due to its high mechanical strength. The steel's resistance to hydrogen embrittlement is critical in downhole environments where exposure to hydrogen sulfide (H₂S) can lead to material degradation and failure.
American musical instrument string producer Ernie Ball has made a specialist type of electric guitar string out of maraging steel, claiming that this alloy provides more output and enhanced tonal response.
The production, import, and export of maraging steels by certain entities, such as the United States, is closely monitored by international authorities because it is particularly suited for use in gas centrifuges for uranium enrichment; lack of maraging steel significantly hampers the uranium-enrichment process. Older centrifuges used aluminum tubes, while modern ones use carbon fiber composite.
Physical properties
- Density: 8.1 g/cm<sup>3</sup> (0.29 lb/in<sup>3</sup>)
- Specific heat, mean for 0–100 °C (32–212 °F): 452 J/kg·K (0.108 Btu/lb·°F)
- Melting point:
- Thermal conductivity: 25.5 W/m·K
- Mean coefficient of thermal expansion: 11.3×10<sup>−6</sup> K<sup>−1</sup> (20.3×10<sup>−6</sup> °F<sup>−1</sup>)
- Yield tensile strength: typically
- Ultimate tensile strength: typically . Grades exist up to
- Elongation at break: up to 15%
- K<sub>IC</sub> fracture toughness: up to 175 MPa·m<sup></sup>
- Young's modulus:
- Shear modulus:
- Bulk modulus:
- Hardness (aged): 50 HRC (grade 250); 54 HRC (grade 300); 58 HRC (grade 350)
See also
- Aermet
- USAF-96 and Eglin steel (Inexpensive maraging steels with less nickel and other expensive materials.)
References
External links
- Maraging steel data sheets
