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Carpenter Custom 455® Stainless Steel, Condition H1000 (Age Hardened 538°C (1000°F))
Categories: Metal; Ferrous Metal; Stainless Steel; T 400 Series Stainless Steel

Material Notes: Data provided by Carpenter Technology Corporation.

Recognizing the need for high-strength alloys with good corrosion resistance to atmospheric environments, the Carpenter Research Laboratory developed Custom 455® stainless, a martensitic age-hardenable stainless steel. This alloy is relatively soft and formable in the annealed condition. A single-step aging treatment develops exceptionally high yield strength with good ductility and toughness. This stainless can be machined in the annealed condition, and welded in much the same manner as other precipitation hardenable stainless steels. Because of its low work-hardening rate, it can be extensively cold formed. The dimensional change during hardening is only about -0.001 in/in, which permits close-tolerance finish machining in the annealed state. Custom 455 stainless represents a significant advancement in the area of precipitation hardening stainless steels. It should be considered where simplicity of heat treatment, ease of fabrication, high strength and corrosion resistance are required in combination.

Because of the unique combination of high strength and corrosion resistance of Custom 455 stainless there are few other alloys available for consideration. Carpenter PH13-8 Mo can be considered where good transverse toughness and ductility are necessary in large sections.

Custom 455® is a registered trademark of Carpenter Technology Corporation.

Key Words: UNS S45500
Vendors: Visit metalmen for your metals needs. Products include special chemistry, tight tolerances, custom tempers, odd dimensions/forms, and small quantities. Phone 1-800-767-9494.

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Physical PropertiesOriginal ValueComments
Density 7.76 g/cc
 
Mechanical PropertiesOriginal ValueComments
Hardness, Brinell 411Estimated from Rockwell C for 3000 kg load, 10 mm ball Brinell measurement.
Hardness, Knoop 450Estimated from Rockwell C
Hardness, Rockwell C 44
Hardness, Vickers 430Estimated from Rockwell C
Tensile Strength, Ultimate 1413 MPa
 814 MPa
@Temperature 538 °C
 1062 MPa
@Temperature 427 °C
 1200 MPa
@Temperature 316 °C
 1517 MPa
@Temperature -73.0 °C
 1758 MPa
@Temperature -184 °C
Tensile Strength, Yield 1345 MPa
@Strain 0.2 %
 138 MPa
@Strain 0.2 %,
Temperature 316 °C
 738 MPa
@Strain 0.2 %,
Temperature 538 °C
 1020 MPa
@Strain 0.2 %,
Temperature 427 °C
Elongation at Break 14 %In 4D
 13 %
@Temperature -73.0 °C
 13 %
@Temperature -184 °C
 14 %
@Temperature 316 °C
In 4D
 15 %
@Temperature 427 °C
In 4D
 20 %
@Temperature 538 °C
In 4D
Reduction of Area 55 %
 45 %
@Temperature -184 °C
 50 %
@Temperature -73.0 °C
 60 %
@Temperature 316 °C
 65 %
@Temperature 427 °C
 75 %
@Temperature 538 °C
Modulus of Elasticity 200 GPa
Notched Tensile Strength 1517 MPa
@Temperature -184 °C
 2000 MPa
@Temperature 23.0 °C
 2070 MPa
@Temperature -73.0 °C
Poissons Ratio 0.30
Fatigue Strength 630 MPa
@# of Cycles 1.00e+7
R.R. Moore Test, Smooth Rotating Beam
Shear Modulus 76.9 GPaCalculated
Charpy Impact 30.0 JV-notch
 5.00 J
@Temperature -184 °C
V-notch
 16.0 J
@Temperature -73.0 °C
V-notch
 
Electrical PropertiesOriginal ValueComments
Electrical Resistivity 0.0000758 ohm-cm
@Temperature 23.0 °C
 
Thermal PropertiesOriginal ValueComments
CTE, linear 10.6 µm/m-°C
@Temperature 22.0 - 93.0 °C
 11.2 µm/m-°C
@Temperature 22.0 - 260 °C
 12.0 µm/m-°C
@Temperature 22.0 - 482 °C
 
Component Elements PropertiesOriginal ValueComments
Carbon, C <= 0.050 %
Chromium, Cr 11 - 12.5 %
Copper, Cu 1.5 - 2.5 %
Iron, Fe 75 %as remainder
Manganese, Mn <= 0.50 %
Molybdenum, Mo <= 0.50 %
Nb + Ta 0.10 - 0.50 %
Nickel, Ni 7.5 - 9.5 %
Niobium, Nb (Columbium, Cb) <= 0.50 %
Phosphorus, P <= 0.040 %
Silicon, Si <= 0.50 %
Sulfur, S <= 0.030 %
Tantalum, Ta <= 0.50 %
Titanium, Ti 0.80 - 1.4 %

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