SAE 5950 Nickel Alloys

Material group: Nonferrous Alloys / Nickel Alloys
Country / Standard: United States / SAE

Data updates

Latest Update: 2020-11
Total number of updates: 2
Update History
2014-10

This material has 51 properties — only a subset is shown here.

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SAE 5950 Chemical Composition

CRITERIA
VALUE
UNIT
CAS NUMBER
CRITERIA
Al
VALUE
0.20 – 0.80
UNIT
%
CAS NUMBER
7429-90-5
CRITERIA
B
VALUE
≤ 0.006
UNIT
%
CAS NUMBER
7440-42-8
CRITERIA
C
VALUE
≤ 0.05
UNIT
%
CAS NUMBER
7440-44-0
CRITERIA
Co
VALUE
val1
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UNIT
%
CAS NUMBER
7440-48-4
CRITERIA
Cr
VALUE
val1
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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
Nb
VALUE
val1
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UNIT
%
CAS NUMBER
7440-03-1
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

SAE AMS 5950E: 2025 / Nickel Alloy, Corrosion- and Heat-Resistant, Sheet and Strip, 52.5Ni - 19Cr - 3.0Mo - 5.0Cb (Nb) - 0.90Ti - 0.50AI - 18Fe (Inconel 718SPF), Vacuum Induction and Consumable Electrode Remelted, Solution Heat Treated, Precipitation Hardenable

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SAE 5950 Physical Properties


Temperature

PROPERTY / VALUE
Modulus of Elasticity
185 — 205 GPa
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Density
7.9 — 8.8 kg/dm³
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Poisson Coefficient
0.32 — 0.34
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This material has 51 properties — only a subset is shown here.

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SAE 5950 Heat Treatments


  • Solution heat treated in a suitable protective atmosphere, preferably in hydrogen or argon or in a vacuum to a temperature within the range 927 to 996°C (1700 to 1825°F), holding at the selected temperature within ±14°C (±25°F) for a time commensurate with product thickness, and cooling at a rate equivalent to an air cool or faster.
    After Precipitation Heat Treatment by heating to 718°C ± 8°C (1325°F ± 15°F), holding at heat for 8 hours ± 0.5 hour, cooling at 56°C ± 8°C (100°F ± 15°F) degrees per hour to 621°C ± 8°C (1150°F ± 15°F), holding at 621°C ± 8°C (1150°F ± 15°F) for 8 hours ± 0.5 hour, and cooling in air. Instead of the 56°C ± 8°C (100°F ± 15°F) degrees per hour cooling rate to 621°C ± 8°C (1150°F ± 15°F), product may be furnace cooled at any rate provided the time at 621°C ± 8°C (1150°F ± 15°F) is adjusted to give a total precipitation heat treatment time of 18 hours. After being re-solution heat treated by heating to 954°C ± 14°C (1750°F ± 25°F), holding at heat for 60 minutes ± 5 minutes, and cooling at a rate equivalent to an air cool or faster and precipitation heat treated as above.

SAE 5950 Mechanical Properties


Temperature

PROPERTY / VALUE
Tensile Strength
1241 — 1276 MPa
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Elongation, A
≥ 12 %
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Yield Strength, Rp0.2
val1
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MPa
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Grain Size
val1
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Rockwell Hardness (HR)
val1
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SAE 5950 International Equivalent Materials


Showing 3 of 3 results.

MATERIAL
STANDARD
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
MATERIAL
STANDARD
UNS
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Official
STANDARD
PROPRIETARY
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
Official
MATERIAL
STANDARD
SAE
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Implicit

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  • 3Cross References

  • 16Composition
  • 22Mechanical Properties
  • 3Physical Properties
  • 1Heat Treatment
  • -Metallography
  • -Machinability

  • -Stress-Strain
  • 1Formability
  • -Fatigue
  • -Fracture
  • 3Creep

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

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

  • 2Total Suppliers