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PH13-8Mo / X3CrNiMoAl13-8-2

1.4534
Stainless Steelph
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Premium aerospace precipitation-hardening stainless. Al-precipitation for the highest transverse toughness and most uniform properties of all PH stainless grades. SCC-resistant in marine environments. Used for landing gear, structural airframe parts, nuclear components, and high-performance shafts.

International equivalents

FlagStandardCountryGradeNumberMatch
🇺🇸AMSUSAUNS S13800S13800REF
🇪🇺ENEuropeX3CrNiMoAl13-8-21.453495%

Sources: AMS 5629, EN 10088-3

Chemical composition comparison (wt%)

Side-by-side: PH13-8Mo / X3CrNiMoAl13-8-2 (ASTM) (AMS 5629) vs X3CrNiMoAl13-8-2 (EN)

ElementPH13-8Mo / X3CrNiMoAl13-8-2 (ASTM)X3CrNiMoAl13-8-2 (EN)Overlap
C0–0.05%——
Si0–0.1%——
Mn0–0.1%——
Cr12.25–13.25%——
Mo2–2.5%——
Ni7.5–8.5%——
Al0.9–1.35%——
N0–0.01%——

Mechanical properties

H950

PropertyValueUnit
Tensile Strength≥ 1410MPa
Yield Strength≥ 1310MPa
Elongation≥ 8%
Hardness HRC44–48HRC
Elastic Modulus≥ 196GPa
Density≥ 7.76g/cm3

H1000

PropertyValueUnit
Tensile Strength≥ 1275MPa
Yield Strength≥ 1170MPa

Heat treatment

ProcessTemperatureMediumHolding TimeNotes
solution_treating925–950 °Cair30-60 minCool to -73°C within 24h for martensite completion
aging_H950510–510 °Cair4 hoursH950: Peak strength (1410 MPa UTS)
aging_H1000540–540 °Cair4 hoursH1000: Better toughness

Compatibility verdict

PH13-8Mo / X3CrNiMoAl13-8-2 and X3CrNiMoAl13-8-2: 95% composition match

Close equivalents but NOT identical.

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All data is for reference only. Equivalents indicate similarity, not identity. Always verify against the applicable specification for safety-critical applications. materialref.com accepts no liability for decisions based on this data.