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title: "X6NiCrTiMoV26-15"
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DIN / EN · Europe · 15 designations

# X6NiCrTiMoV26-15

X6NiCrTiMoV26-15 is a material in the category [High-temperature steels](/categories/high-temperature-steels "High-temperature steels") / aviation variant, held under material number 1.4944. We list 14 designations recorded for this grade, in the standards UNS, AISI / SAE, ASTM and SAE AMS. Its recorded composition includes C ≤ 0.08%, Ti 1.9–2.3%, Cr 13.5–16%, Mn ≤ 2% and Ni 24–27%. Its recorded density is 7.95 g/cm³.

- [*Material no.* **1.4944**](/materials/material-no/1.4944 "Material no.: 1.4944")
- [*Category* **High-temperature steels / aviation variant · 12 grades**](/categories/high-temperature-steels-aviation-variant "Category: High-temperature steels / aviation variant · 12 grades")
- *Designations* **15**

[Search](/search "Steel grade search")[Inquiry](/inquiry?material=93118751-9123-4efa-b870-8ed70c6e2a7e&designation=f217e34a-d632-4985-908d-e115f33c59ab "Inquiry")[**Datasheet as PDF** Print-ready A4 document **Generating …** **Download started** **Try again**](/materials/din-en/x6nicrtimov26-15.pdf "Datasheet as PDF")

## If you came for one of these

 The most-used names for this grade.

- [UNS S66286 This grade’s own name · 6 grades on that route](/materials/uns/s66286 "UNS S66286")
- [AISI / SAE 660 This grade’s own name · 5 grades on that route](/materials/aisi-sae/660 "AISI / SAE 660")

## 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

 15 designations · 5 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Withdrawn designation no longer current — a separate column from the two above, so a name can be same grade and withdrawn at once.

DIN / EN Europe · 1

- **X6NiCrTiMoV26-15 This grade’s own name**

UNS United States · 1

- [S66286 This grade’s own name](/materials/uns/s66286 "UNS S66286")

AISI / SAE United States · 1

- [660 This grade’s own name](/materials/aisi-sae/660 "AISI / SAE 660")

ASTM United States · 2

- [A453 Indicative](/materials/astm/a453 "ASTM A453")
- [A638 Indicative](/materials/astm/a638 "ASTM A638")

SAE AMS United States / Aerospace · 10

- [5525 Indicative plate sheet](/materials/ams/5525 "SAE AMS 5525")
- [5723 Indicative](/materials/ams/5723 "SAE AMS 5723")
- [5726 Indicative bar](/materials/ams/5726 "SAE AMS 5726")
- [5731 Indicative bar](/materials/ams/5731 "SAE AMS 5731")
- [5732 Indicative bar](/materials/ams/5732 "SAE AMS 5732")
- [5734 Indicative bar](/materials/ams/5734 "SAE AMS 5734")
- [5737 Indicative bar](/materials/ams/5737 "SAE AMS 5737")
- [5853 Indicative bar](/materials/ams/5853 "SAE AMS 5853")
- [5858 Indicative sheet strip](/materials/ams/5858 "SAE AMS 5858")
- [5895 Indicative bar](/materials/ams/5895 "SAE AMS 5895")

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 Ni Cr Ti

Iron — the balance, never listed by a standard — 52.6 % Ni — 25.5 % Cr — 14.8 % Ti — 2.1 % Traces & impurities · 5 %

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

| Element | % by weight |
|---|---|
| C | ≤ 0.08 |
| Si | ≤ 1 |
| Mn | ≤ 2 |
| P | 0.025 |
| S | 0.015 |
| Cr | 13.5–16 |
| Mo | 1–1.5 |
| Ni | 24–27 |
| V | 0.1–0.5 |
| Al | ≤ 0.35 |
| Ti | 1.9–2.3 |
| B | 0.003–0.01 |

Carbon Silicon Manganese Phosphorus Sulfur Chromium Molybdenum Nickel Vanadium Aluminium Titanium Boron

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 |
|---|---|---|---|---|
| B | 0,003-0,010 | 0.003 | 0.010 | Range |
| C | ≤0,08 | — | 0.080 | Max |
| Al | ≤0,35 | — | 0.350 | Max |
| Si | ≤1,00 | — | 1.000 | Max |
| P | 0,025 | 0.025 | 0.025 | Exact |
| S | 0,015 | 0.015 | 0.015 | Exact |
| Ti | 1,90-2,30 | 1.900 | 2.300 | Range |
| V | 0,10-0,50 | 0.100 | 0.500 | Range |
| Cr | 13,5-16,0 | 13.500 | 16.000 | Range |
| Mn | ≤2,00 | — | 2.000 | Max |
| Ni | 24,0-27,0 | 24.000 | 27.000 | Range |
| Mo | 1,00-1,50 | 1.000 | 1.500 | 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 7,95 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=93118751-9123-4efa-b870-8ed70c6e2a7e&designation=f217e34a-d632-4985-908d-e115f33c59ab "Inquiry")[**Datasheet as PDF** Print-ready A4 document **Generating …** **Download started** **Try again**](/materials/din-en/x6nicrtimov26-15.pdf "Datasheet as PDF")
