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Maraging Steel C300

Maraging Steel

Basic Information

Category: Maraging Steel
Material Type: alloy
Alternative Names:
C30018Ni(300)Grade 300UNS K93120AMS 6514
Tags:
maragingprecipitation-hardeneddefenseultra-high-strengthnickel-steel

Composition & Structure

Composition: Fe-18Ni-9Co-4.8Mo-0.6Ti-0.1Al
Microstructure: Lath martensite matrix with Ni₃(Mo,Ti) precipitates at higher volume fraction than C250; NO carbides. Prior austenite grain boundaries. Reverted austenite possible if over-aged.

Description

Maraging Steel C300 is the higher-strength variant of the 18Ni maraging steel family, achieving ~54 HRC through a higher volume fraction of Ni3(Mo,Ti) intermetallic precipitates. No carbides. Used in defense and aerospace where ultra-high strength with good toughness is required.

Mechanical Properties

Hardness: 54 HRC
Hardness (HB): 530 HB
Hardness (HRC): 54 HRC
Hardness (HV): 577 HV
Hardness Category: hard
Tensile Strength: 2050 MPa
Yield Strength: 1990 MPa

Physical Properties

Density: 8.0 g/cm³
Melting Point: 1430 °C

Material Characteristics

Work Hardening: No
Magnetic: Yes
Corrosion Resistance: low

General Preparation Notes

Maraging Steel C300 is an ultra-high-strength (54 HRC aged, ~577 HV) precipitation-hardened nickel steel with a density of 8.0 g/cm³. The microstructure is the same type as C250 (lath martensite with Ni₃(Mo,Ti) precipitates, no carbides) but with a higher precipitate volume fraction producing greater hardness. Preparation is essentially the same as C250, with allowance for the increased hardness during grinding and cutting.

Sectioning

Use an abrasive cut-off wheel designed for hardened steel (aluminum oxide abrasive). Standard wheel thickness (1.0-1.5 mm). Cutting speed: 200-300 RPM with generous coolant flow. The higher hardness (~54 HRC) compared to C250 means slightly slower cutting rates. Do not force the cut; allow the wheel to work at its own rate. Excessive heat will alter the precipitation state. Leave 2-3 mm allowance for grinding away the heat-affected zone.

Mounting

Hot compression mounting with phenolic or epoxy-phenolic resin is acceptable. The aging temperature (480°C) is well above mounting temperatures (150-180°C), so no microstructural change occurs during mounting. Cold mounting with castable epoxy is equally suitable. Standard mounting practices apply.

Grinding

The higher hardness (54 HRC, ~577 HV) compared to C250 means slightly more abrasive wear during grinding, but the technique is the same. Use SiC grinding papers with abundant water lubrication. Disc speed: 250-300 RPM. Apply moderate pressure (25-35 N per 30 mm sample).

Grinding sequence:
  • 120 grit: Remove sectioning damage and heat-affected zone (30-60 seconds). Moderate pressure.
  • 240 grit: Remove previous scratches (20-40 seconds).
  • 320 grit: Refinement (20-40 seconds).
  • 400 grit: Further refinement (20-40 seconds).
  • 600 grit: Final grinding (20-40 seconds).
Rotate specimen 90° between steps. Use complementary rotation. The single-phase martensite grinds uniformly without differential removal.
Recommended Sequence:
120240320400600

Polishing

Same approach as C250. The uniform martensite structure polishes well without relief.

Diamond polishing sequence:
  • 6μm diamond: 3-5 minutes on a medium-hard synthetic pad with moderate pressure (25-35 N per 30 mm sample).
  • 1μm diamond: 2-4 minutes on a synthetic pad (20-30 N).
Final polishing:
  • 0.05μm colloidal silica: 1-3 minutes on a soft final polishing pad (15-20 N). Colloidal silica provides effective chemical-mechanical action for revealing lath martensite in maraging steels.
Recommended Sequence:
6μm diamond1μm diamond0.05μm colloidal silica

Etching

Same etchants as C250. The microstructure is the same type but with a higher precipitate volume fraction.

Modified Fry's Reagent (Chemical Etching) - Primary choice:
  • Composition: 5 g CuCl₂, 40 ml HCl, 30 ml H₂O, 25 ml ethanol
  • Application: Immerse for 10-30 seconds or swab.
  • Reveals: Lath martensite, prior austenite grain boundaries, reverted austenite.
  • Rinse: Water, then ethanol. Dry with warm air.
2% Nital (Chemical Etching) - General purpose:
  • Composition: 2 ml HNO₃, 98 ml ethanol
  • Application: Immerse for 5-15 seconds.
  • Reveals: General martensitic structure and prior austenite grain boundaries.
Note: As with C250, the Ni₃(Mo,Ti) precipitates are nanoscale and require TEM for direct observation.
Common Etchants:
Modified Fry's Reagent2% Nital

Heat Treatment

Solution treated at 820°C, air cooled; aged at 480°C for 3-6 hours

ASTM Standards

  • ASTM A538

Applications

  • Defense
  • Pressure vessels
  • Aircraft forgings
  • Submarine hulls

Typical Uses

  • Missile casings
  • Pressure vessel shells
  • Aircraft structural forgings
  • Submarine hull components