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High-temperature steels / aviation variant
Category · 12 grades

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.

GradeMaterial no.CSiPSCrMn
X8CrCoNiMo10-61.49110,05-0,120,10-0,800,0250,0159,80-11,20,30-1,30
1.49141.49140,11-0,190,15-0,650,030,02510,0-12,00,20-1,25
1.49341.49340,18-0,260,15-0,400,0350,03510,5-12,50,40-0,70
X12CrNiMo121.49390,08-0,13≤0,350,0250,0211,0-12,50,50-0,90
X6NiCrTiMoV26-151.4944≤0,08≤1,000,0250,01513,5-16,0≤2,00
R301551.49740,08-0,16≤1,000,040,0320,0-22,51,00-2,00
S316001.49840,04-0,100,30-0,600,0450,0315,5-17,5≤1,50
NiCr20Ti2.46300,08-0,15≤1,000,030,0218,0-21,0≤1,00
NiCr20TiAl2.46310,04-0,10≤1,000,030,01518,0-21,0≤1,00
NiCr20Co18Ti2.4632≤0,13≤1,000,020,01518,0-21,0≤1,00
NiCo20Cr15MoAlTi2.46340,12-0,17≤1,000,0450,01514,0-15,7≤1,00
CoCr20W15Ni2.49640,05-0,15≤0,400,020,01519,0-21,0≤2,00

Standards covering this category

11

Property ranges

3
PropertyUnitMinMaxGrades
HB2302301
HRC32321
rhog/cm³7.859.112

Derived from 12 grades in this category with a recorded value.

Composition range

20
PropertyUnitMinMaxGrades
B%0.0030.025
C%0.040.2612
N%0.020.24
Al%0.354.94
Si%0.1112
P%0.020.04512
S%0.0150.03512
Ti%0.235
V%0.10.75
Cr%9.822.512
Mn%0.2212
Fe%155
Co%257.9157
Ni%0.281.6712
Cu%0.20.54
Zr%0.150.152
Nb%0.11.253
Mo%0.45.58
W%0.4164
Pb%0.0050.0051

Derived from 12 grades in this category with a recorded value.

Related guides

3