MIL C81500 Copper Alloys

Material group: Nonferrous Alloys / Copper Alloys
Country / Standard: United States / MIL

Data updates

Latest Update: 2014-08
Total number of updates: 1
Update History

This material has 17 properties — only a subset is shown here.

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MIL C81500 Chemical Composition

CRITERIA
VALUE
UNIT
CAS NUMBER
CRITERIA
Cr
VALUE
0.4000 – 1.5000
UNIT
%
CAS NUMBER
7440-47-3
CRITERIA
Cu
VALUE
≥ 98.0000
UNIT
%
CAS NUMBER
7440-50-8
CRITERIA
Other total
VALUE
≤ 0.5000
UNIT
%
CAS NUMBER

MIL-C-19310A: 1972 / Copper-chromium-alloy castings

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MIL C81500 Physical Properties


Temperature

PROPERTY / VALUE
Modulus of Elasticity
100 — 150 GPa
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Density
7.5 — 9.3 kg/dm³
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This material has 17 properties — only a subset is shown here.

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MIL C81500 Mechanical Properties


Temperature

PROPERTY / VALUE
Tensile Strength
≥ 276 MPa
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Brinell Hardness (HB)
≥ 89
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Elongation, A
≥ 15 %
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Rockwell Hardness (HR)
val1
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Yield Strength, Rp0.2
val1
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MPa
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MIL C81500 International Equivalent Materials


Showing 5 of 5 results.

MATERIAL
STANDARD
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
MATERIAL
STANDARD
UNS
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Official
MATERIAL
STANDARD
AS
COUNTRY / PRODUCER
Australia
EQUIVALENCE CATEGORY
Implicit
MATERIAL
STANDARD
AS
COUNTRY / PRODUCER
Australia
EQUIVALENCE CATEGORY
Implicit
MATERIAL
STANDARD
CDA
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Implicit
MATERIAL
STANDARD
PROPRIETARY
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
Implicit

Equivalence categories reflect chemical-composition and mechanical-property comparison — always verify suitability against the governing specification for your application.

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  • 5Cross References

  • 3Composition
  • 5Mechanical Properties
  • 2Physical Properties
  • -Heat Treatment
  • -Metallography
  • -Machinability

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

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

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

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