T1-5
T1-50 · other
T1-50
| ASTM A463 / A463M
C 0.15 max Mn 0.60 max (Type 1); Al-Si coating
T1-6
T1-60 · other
T1-60
| ASTM A463 / A463M
C 0.15 max Mn 0.60 max (Type 1); Al-Si coating
T10
T10 · other
T10
Wire | T 1298 T10
C:0.95-1.05;Si:0.15-0.35;Mn:0.25-0.45;Cr:1.40-1.65
T100
T100 · alloy
T100
Bar,Plate |
C:0.30-0.45;Mn:0.60-1.00;Si:0.15-0.35;Cr:0.50-1.00;P:≤0.035;S:≤0.040
T105
T105 · alloy
T105
Bar,Plate |
C:0.30-0.45;Mn:0.60-1.00;Si:0.15-0.35;Cr:0.50-1.00;P:≤0.035;S:≤0.040
T10A
T10A · alloy
T10A / T00103
Bar, Plate, Tube, Forging, Wire |
C:0.95-1.04;Si:≤0.35;Mn:≤0.4;P:≤0.03;S:≤0.02;Cr:≤0.25;Ni:≤0.2;Cu:≤0.25
T11
T11 · alloy
T11
Bar,Plate | ASTM A213 T11, ASME SA-213 / SA-213M; ASTM A213, ASTM A250 / A250M
C:0.30-0.45;Mn:0.60-1.00;Si:0.15-0.35;Cr:0.50-1.00;P:≤0.035;S:≤0.040
T110
T110 · alloy
T110
Bar,Plate |
C:0.30-0.45;Mn:0.60-1.00;Si:0.15-0.35;Cr:0.50-1.00;P:≤0.035;S:≤0.040
T110
T110-40 · other
T110-40
| ASTM A463 / A463M
C 0.20 max Mn 1.35 max (Type 2); Al-Si coating
T110
T110-50 · other
T110-50
| ASTM A463 / A463M
C 0.20 max Mn 1.35 max; Al-Si coating
T110
T110-60 · other
T110-60
| ASTM A463 / A463M
C 0.20 max Mn 1.35 max; Al-Si coating
T115
T115 · alloy
T115
Bar,Plate |
C:0.30-0.45;Mn:0.60-1.00;Si:0.15-0.35;Cr:0.50-1.00;P:≤0.035;S:≤0.040
T12
T12 · alloy
T12
Bar,Plate | ASTM A213 T12, ASME SA-213 / SA-213M; ASTM A213, ASTM A250 / A250M
C:0.30-0.45;Mn:0.60-1.00;Si:0.15-0.35;Cr:0.50-1.00;P:≤0.035;S:≤0.040
T120
T120 · alloy
T120
Bar,Plate |
C:0.30-0.45;Mn:0.60-1.00;Si:0.15-0.35;Cr:0.50-1.00;P:≤0.035;S:≤0.040
T122
T122 · alloy
T122
Bar,Plate | ASTM A213 T122, ASME SA-213 / SA-213M; ASTM A213
C:0.30-0.45;Mn:0.60-1.00;Si:0.15-0.35;Cr:0.50-1.00;P:≤0.035;S:≤0.040
T13
T13 · other
T13
Wire | T 1298 T13
C:0.95-1.05;Si:0.15-0.35;Mn:0.25-0.45;Cr:1.40-1.65
T135
T135 · alloy
T135
Bar,Plate |
C:0.30-0.45;Mn:0.60-1.00;Si:0.15-0.35;Cr:0.50-1.00;P:≤0.035;S:≤0.040
T15
T15 · other
T15
Nickel/cobalt-base superalloy retaining high strength, creep and corrosion resistance at extreme temperature. Cobalt (≈5%) raises hot corrosion and wear resistance. Used in gas-turbine blades, aero-engine hot sections, combustors and advanced energy syste | ASTM A600 T15
C:1.50-1.60;W:11.0-13.0;Cr:3.75-5.00;V:4.50-5.25;Co:4.75-5.25;P:≤0.030;S:≤0.030
T150
T150 · alloy
T150
Bar,Plate |
C:0.30-0.45;Mn:0.60-1.00;Si:0.15-0.35;Cr:0.50-1.00;P:≤0.035;S:≤0.040