PROPRIETARY ATI S240 Alloy Stainless steels

Material group: Ferrous Alloys / Stainless steels
Country / Standard: PROPRIETARY

Data updates

Latest Update: 2026-02
Total number of updates: 3
Update History
2022-11 2021-03

This material has 154 properties — only a subset is shown here.

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PROPRIETARY ATI S240 Alloy Chemical Composition

CRITERIA
VALUE
UNIT
CAS NUMBER
CRITERIA
Al
VALUE
0.7 – 1.5
UNIT
%
CAS NUMBER
7429-90-5
CRITERIA
C
VALUE
≤ 0.03
UNIT
%
CAS NUMBER
7440-44-0
CRITERIA
Cr
VALUE
11.00 – 12.50
UNIT
%
CAS NUMBER
7440-47-3
CRITERIA
Cu
VALUE
val1
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UNIT
%
CAS NUMBER
7440-50-8
CRITERIA
Fe
VALUE
val1
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UNIT
%
CAS NUMBER
7439-89-6
CRITERIA
Mn
VALUE
val1
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UNIT
%
CAS NUMBER
7439-96-5
CRITERIA
Mo
VALUE
val1
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UNIT
%
CAS NUMBER
7439-98-7
CRITERIA
N
VALUE
val1
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UNIT
%
CAS NUMBER
7727-37-9; 17778-88-0
CRITERIA
Ni
VALUE
val1
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UNIT
%
CAS NUMBER
7440-02-0
CRITERIA
P
VALUE
val1
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UNIT
%
CAS NUMBER
7723-14-0
CRITERIA
S
VALUE
val1
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UNIT
%
CAS NUMBER
7704-34-9
CRITERIA
Si
VALUE
val1
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UNIT
%
CAS NUMBER
7440-21-3
CRITERIA
Ti
VALUE
val1
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UNIT
%
CAS NUMBER
7440-32-6
CRITERIA
W
VALUE
val1
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UNIT
%
CAS NUMBER
7440-33-7

Allegheny Technologies Incorporated, Product Data Sheets,

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PROPRIETARY ATI S240 Alloy Physical Properties


Temperature

PROPERTY / VALUE
Modulus of Elasticity
179.3 — 215 GPa
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Thermal Conductivity
14.954 W/(m∙°C)
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Density
val1
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kg/dm³
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Heat Capacity
val1
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J/(kg∙°C)
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Melting Temperature
val1
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°C
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Poisson Coefficient
val1
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This material has 154 properties — only a subset is shown here.

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PROPRIETARY ATI S240 Alloy Heat Treatments


  • Solution treatment should be performed from 913ºC to 941ºC (1675ºF to 1725ºF) for 45 to 75 minutes at temperature followed by cooling to 0ºC (32ºF) and holding for at least four hours to ensure complete transformation to martensite. No “deep freeze” or cryogenic processing is required. Aging is normally carried out from 510ºC to 621ºC (950ºF to 1150ºF), depending upon the desired final properties. Heat treatment is usually performed in air. Heat treatment of brazed components may be done in inert atmospheres. Reducing atmospheres should not be used because of the potential for nitrogen contamination.

PROPRIETARY ATI S240 Alloy Mechanical Properties


Temperature

PROPERTY / VALUE
Tensile Strength
1172 — 1704.1 MPa
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Elongation, A
val1
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%
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Reduction of Area
val1
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%
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Yield Strength, Rp0.2
val1
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MPa
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Impact Energy
val1
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J
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  • 3Cross References

  • 14Composition
  • 96Mechanical Properties
  • 33Physical Properties
  • 1Heat Treatment
  • -Metallography
  • -Machinability

  • 4Stress-Strain
  • -Formability
  • -Fatigue
  • 2Fracture
  • -Creep

  • -Joints
  • -Coatings
  • -Dimensions
  • -Tribology

  • -Corrosion
  • -Ageing
  • -Weatherability
  • -Irradiation

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