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SAE AMS · United States / Aerospace · 8 designations

5537

5537 is a designation in SAE AMS for the material held under material number 2.4964, also listed as CoCr20W15Ni. It is a material in the category High-temperature steels / aviation variant. We list 8 designations recorded for this grade, in the standards DIN / EN, UNS, AISI / SAE, ASTM and SAE AMS.

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

8 designations · 5 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Withdrawndesignation no longer current — a separate column from the two above, so a name can be same grade and withdrawn at once.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 · 1
AISI / SAEUnited States · 1
ASTMUnited States · 1
SAE AMSUnited States / Aerospace · 4

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 — 52.5 %Cr — 20 %W — 15 %Ni — 10 %Traces & impurities · 2.5 %

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

Element% by weight
0.05–0.15
≤ 0.4
≤ 2
0.02
0.015
19–21
9–11
14–16 —
Balance
≤ 3
CarbonSiliconManganesePhosphorusSulfurChromiumNickelTungstenCobaltIron
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
C0,05-0,150.0500.150Range
Si≤0,400.400Max
P0,020.0200.020Exact
S0,0150.0150.015Exact
Cr19,0-21,019.00021.000Range
Mn≤2,002.000Max
Fe≤3,003.000Max
CoRest/Bal.46.41557.915Balance
Ni9,00-11,09.00011.000Range
W14,0-16,014.00016.000Range

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

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

Physical & mechanical properties

Density9,1g/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.