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title: "1.4974 — High-temperature steels / aviation variant"
description: "1.4974 is the material number of the grade also listed as R30155. It is a material in the category High-temperature steels / aviation variant."
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Material number · Europe · 5 designations

# 1.4974

1.4974 is the material number of the grade also listed as R30155. It is a material in the category High-temperature steels / aviation variant. We list 5 designations recorded for this grade, in the standards UNS and SAE AMS.

- ***Material no.* **1.4974****
- [*Category* **High-temperature steels / aviation variant · 12 grades**](/categories/high-temperature-steels-aviation-variant "Category: High-temperature steels / aviation variant · 12 grades")
- *Designations* **5**

[Search](/search "Steel grade search")[Inquiry](/inquiry?material=c27c8f33-d1e2-4ed8-a00c-0f87e1dd2d1a "Inquiry")[**Datasheet as PDF** Print-ready A4 document **Generating …** **Download started** **Try again**](/materials/material-no/1.4974.pdf "Datasheet as PDF")

## 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 · 2 standards · nothing hidden

This grade’s own name recorded in our sources as this grade’s own designation under that standard.

Indicative taken from a published cross-reference table; a close match, not a guarantee of interchangeability. Verify against the mill certificate before ordering.

Withdrawn designation no longer current — a separate column from the two above, so a name can be same grade and withdrawn at once.

UNS United States · 1

- [R30155 Indicative](/materials/uns/r30155 "UNS R30155")

SAE AMS United States / Aerospace · 4

- [5532 Indicative plate sheet strip](/materials/ams/5532 "SAE AMS 5532")
- [5769 Indicative bar forging ring](/materials/ams/5769 "SAE AMS 5769")
- [5794 Indicative wire](/materials/ams/5794 "SAE AMS 5794")
- [5795 Indicative](/materials/ams/5795 "SAE AMS 5795")

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

## Chemical composition

 12 elements on file · weight %

What this alloy is

Fe Cr Ni Co

Iron — the balance, never listed by a standard — 29.7 % Cr — 21.3 % Ni — 20 % Co — 19.8 % Traces & impurities · 9.3 %

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

| Element | % by weight |
|---|---|
| C | 0.08–0.16 |
| Si | ≤ 1 |
| Mn | 1–2 |
| P | 0.04 |
| S | 0.03 |
| Cr | 20–22.5 |
| Mo | 2.5–3.5 |
| Ni | 19–21 |
| W | 2–3 |
| Co | 18.5–21 |
| Nb | 0.75–1.25 |
| N | 0.1–0.2 |

Carbon Silicon Manganese Phosphorus Sulfur Chromium Molybdenum Nickel Tungsten Cobalt Niobium Nitrogen

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.

| Element | As published source text, verbatim | Min% by weight | Max% by weight | Bound |
|---|---|---|---|---|
| C | 0,08-0,16 | 0.080 | 0.160 | Range |
| N | 0,10-0,20 | 0.100 | 0.200 | Range |
| Si | ≤1,00 | — | 1.000 | Max |
| P | 0,04 | 0.040 | 0.040 | Exact |
| S | 0,03 | 0.030 | 0.030 | Exact |
| Cr | 20,0-22,5 | 20.000 | 22.500 | Range |
| Mn | 1,00-2,00 | 1.000 | 2.000 | Range |
| Co | 18,5-21,0 | 18.500 | 21.000 | Range |
| Ni | 19,0-21,0 | 19.000 | 21.000 | Range |
| Nb | 0,75-1,25 | 0.750 | 1.250 | Range |
| Mo | 2,50-3,50 | 2.500 | 3.500 | Range |
| W | 2,00-3,00 | 2.000 | 3.000 | Range |

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

Density 7,85 g/cm³ Exact

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.

[Search](/search "Steel grade search")[Inquiry](/inquiry?material=c27c8f33-d1e2-4ed8-a00c-0f87e1dd2d1a "Inquiry")[**Datasheet as PDF** Print-ready A4 document **Generating …** **Download started** **Try again**](/materials/material-no/1.4974.pdf "Datasheet as PDF")
