MIL CP-1 Titanium Alloys

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

Data updates

Latest Update: 2019-04
Total number of updates: 2
Update History
2014-08

This material has 79 properties — only a subset is shown here.

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MIL CP-1 Chemical Composition

CRITERIA
VALUE
UNIT
CAS NUMBER
CRITERIA
C
VALUE
≤ 0.0800
UNIT
%
CAS NUMBER
7440-44-0
CRITERIA
Fe
VALUE
≤ 0.5000
UNIT
%
CAS NUMBER
7439-89-6
CRITERIA
H
VALUE
≤ 0.0150
UNIT
%
CAS NUMBER
1333-74-0
CRITERIA
N
VALUE
val1
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UNIT
%
CAS NUMBER
7727-37-9; 17778-88-0
CRITERIA
O
VALUE
val1
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UNIT
%
CAS NUMBER
7782-44-7; 17778-80-2
CRITERIA
Other each
VALUE
val1
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UNIT
%
CAS NUMBER
CRITERIA
Other total
VALUE
val1
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UNIT
%
CAS NUMBER
CRITERIA
Ti
VALUE
val1
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UNIT
%
CAS NUMBER
7440-32-6

MIL-T-81556A: 1996 / Titanium and titanium alloys, extruded bars and shapes, aircraft quality

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MIL CP-1 Physical Properties


Temperature

PROPERTY / VALUE
Compression Modulus
110 GPa
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Modulus of Elasticity
80 — 130 GPa
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Thermal Conductivity
20.641 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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Shear Modulus
val1
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GPa
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This material has 79 properties — only a subset is shown here.

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MIL CP-1 Mechanical Properties


Temperature

PROPERTY / VALUE
Tensile Strength
≥ 552 MPa
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Elongation, A
≥ 10 %
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Yield Strength, Rp0.2
483 — 655 MPa
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MIL CP-1 International Equivalent Materials


Showing 1 of 12 results.

MATERIAL
STANDARD
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
MATERIAL
STANDARD
SAE
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Composition 100%

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  • 12Cross References

  • 16Composition
  • 12Mechanical Properties
  • 32Physical Properties
  • -Heat Treatment
  • -Metallography
  • -Machinability

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

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

  • -Corrosion
  • 2Ageing
  • -Weatherability
  • -Irradiation

  • 1Total Suppliers