PROPRIETARY ATI 13-8 Alloy Stainless steels

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

Data updates

Latest Update: 2022-11
Total number of updates: 3
Update History
2021-10 2016-12

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PROPRIETARY ATI 13-8 Alloy Chemical Composition

CRITERIA
VALUE
UNIT
CAS NUMBER
CRITERIA
Al
VALUE
0.90 – 1.35
UNIT
%
CAS NUMBER
7429-90-5
CRITERIA
C
VALUE
≤ 0.05
UNIT
%
CAS NUMBER
7440-44-0
CRITERIA
Cr
VALUE
12.25 – 13.25
UNIT
%
CAS NUMBER
7440-47-3
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
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

Allegheny Technologies Incorporated, Product Data Sheets,

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PROPRIETARY ATI 13-8 Alloy Physical Properties


Temperature

PROPERTY / VALUE
Modulus of Elasticity
190 — 215 GPa
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Density
val1
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kg/dm³
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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 119 properties — only a subset is shown here.

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PROPRIETARY ATI 13-8 Alloy Heat Treatments


  • Solution heat treated (Condition A) from 910 to 940°C (1675 to 1725°F) for 15 to 30 minutes. Air cool or oil quench to below 15°C (60°F) to effect complete transformation to martensite. Aging is normally carried out from 510 to 620°C (950 to 1150°F), depending upon the desired final properties. Heat treatment is usually performed in air. Heat treatment of brazed components may be done in inert atmospheres.
    Condition H 950: 510°C ± 5°C (950°F ± 10°F), for 4h ± 0.25h.
    Condition H 1000: 540°C ± 5°C (1000°F ± 10°F), for 4h ± 0.25h.
    Condition H 1025: 550°C ± 5°C (1025°F ± 10°F), for 4h ± 0.25h.
    Condition H 1050: 565°C ± 5°C (1050°F ± 10°F), for 4h ± 0.25h.
    Condition H 1100: 595°C ± 5°C (1100°F ± 10°F), for 4h ± 0.25h.
    Condtition H 1150: 620°C ± 5°C (1150°F ± 10°F), for 4h ± 0.25h.

PROPRIETARY ATI 13-8 Alloy Mechanical Properties


Temperature

PROPERTY / VALUE
Tensile Strength
≥ 931 MPa
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Elongation, A
val1
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%
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Yield Strength, Rp0.2
val1
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MPa
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Reduction of Area
val1
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%
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Rockwell Hardness (HR)
val1
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  • 23Cross References

  • 10Composition
  • 66Mechanical Properties
  • 18Physical Properties
  • 1Heat Treatment
  • -Metallography
  • -Machinability

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

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

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

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