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UNS · United States · 7 designations

K92710

K92710 is a designation in UNS for the material held under material number 1.6359, also listed as X2NiCoMo18-8-5. It is a material in the category Special steels for aviation and aerospace. We list 7 designations recorded for this grade, in the standards DIN / EN, UNS, BS and SAE AMS.

If you came for one of these

The most-used names for this grade.

About Special steels for aviation and aerospace

Special steels for aviation and aerospace are engineered steels designed to provide controlled mechanical properties and reliable performance in demanding service. Their alloying and heat-treatment capabilities support components that require a combination of strength, toughness and fatigue resistance, including aircraft structures and engine parts.

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

Also known as

7 designations · 4 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Withdrawndesignation no longer current — a separate column from the two above, so a name can be same grade and withdrawn at once.
UNSUnited States · 3
BSUnited Kingdom · 1
SAE AMSUnited States / Aerospace · 2

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 — 68.6 %Ni — 18 %Co — 7.8 %Mo — 4.9 %Traces & impurities · 0.8 %

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

Element% by weight
≤ 0.03
≤ 0.1
≤ 0.1
0.01
0.01
4.6–5.2
17–19
7–8.5
0.05–0.15
0.3–0.6
CarbonSiliconManganesePhosphorusSulfurMolybdenumNickelCobaltAluminiumTitanium
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
C≤0,030.030Max
Al0,05-0,150.0500.150Range
Si≤0,100.100Max
P0,010.0100.010Exact
S0,010.0100.010Exact
Ti0,30-0,600.3000.600Range
Mn≤0,100.100Max
Co7,00-8,507.0008.500Range
Ni17,0-19,017.00019.000Range
Mo4,60-5,204.6005.200Range

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

Not enough recorded composition to predict a transformation temperature for this grade — missing: Cr.

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.

Similar grades — and why

Selection rule, stated so you can disagree with it: same number class 1.6, a shared category, and a published range for Ni / Co that overlaps this grade’s. These are neighbours in composition space — they are not equivalents, and none is claimed to be interchangeable with this grade.

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.