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DIN / EN · Europe · 5 designations

X12CrNiMo12

X12CrNiMo12 is a material in the category High-temperature steels / aviation variant, held under material number 1.4939. Its recorded composition includes C 0.08–0.13%, Cr 11–12.5%, Mn 0.5–0.9%, Ni 2–3% and Mo 1.5–2%. We list 4 designations recorded for this grade, in the standards DIN / EN, UNS and AISI / SAE. Its recorded density is 7.85 g/cm³.

If you came for one of these

The most-used names for this grade.

About High-temperature steels / aviation variant

High-temperature aviation steels are heat-resistant materials designed to retain strength and structural stability during prolonged exposure to elevated temperatures. Their alloying provides resistance to creep, oxidation, and thermal degradation, making them suitable for aircraft engine and other hot-section components.

This describes the material class as a whole. Always confirm the individual grade against the standard before ordering.

Also known as

5 designations · 3 standards · nothing hidden
This grade’s own namerecorded in our sources as this grade’s own designation under that standard.
Indicativetaken from a published cross-reference table; a close match, not a guarantee of interchangeability. Verify against the mill certificate before ordering.
Withdrawndesignation no longer current — a separate column from the two above, so a name can be same grade and withdrawn at once.
DIN / ENEurope · 2
AISI / SAEUnited States · 1

Every designation on file is listed — no truncation, no “+ n more”. Each one is itself a route that leads back here.

Chemical composition

10 elements on file · weight %

What this alloy is

Iron — the balance, never listed by a standard — 82.4 %Cr — 11.8 %Ni — 2.5 %Mo — 1.8 %Traces & impurities · 1.6 %

Logarithmic scale, 0.01 % to 100 % — every value here compares directly, decade by decade.

Element% by weight
0.08–0.13
≤ 0.35
0.5–0.9
0.025
0.02
11–12.5
1.5–2
2–3
0.25–0.4
0.02–0.04
CarbonSiliconManganesePhosphorusSulfurChromiumMolybdenumNickelVanadiumNitrogen
0.01 %0.1 %1 %10 %100 %

The scale is logarithmic, not the element’s raw share of the alloy — the only honest way to fit 0.01 % and 100 % in one picture, and it means every value here can be compared with every other.

ElementAs publishedsource text, verbatimMin% by weightMax% by weightBound
C0,08-0,130.0800.130Range
N0,020-0,0400.0200.040Range
Si≤0,350.350Max
P0,0250.0250.025Exact
S0,020.0200.020Exact
V0,25-0,400.2500.400Range
Cr11,0-12,511.00012.500Range
Mn0,50-0,900.5000.900Range
Ni2,00-3,002.0003.000Range
Mo1,50-2,001.5002.000Range

The published column is the source string byte-for-byte, decimal comma and all; Min and Max are the parsed bounds. Elements not listed have no value on file — they are omitted, never inferred.

Predicted transformation temperatures

This grade's composition falls outside the published model's validated range (a low-alloy composition window), so no transformation temperature is predicted here.

Physical & mechanical properties

Density7,85g/cm³Exact

An absent property means we hold no value for it — it is left out rather than estimated, interpolated from a neighbouring grade, or filled from a handbook. It does not mean the property is undefined for the material.

Looking for this grade under another name?

Search the catalogue by designation, material number or composition — every name on this page is itself a way in.