Ti-P63002 (European Union / EN) Material Properties

Material group: Nonferrous Alloys / Titanium / Titanium Alloys
Country/Standard: European Union / EN

Data updates

Latest Update: -
Total number of updates: 0
Update History:
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Mechanical Properties

Temperature

0 - 30°C
PROPERTY / VALUE
Yield Strength, Rp0.2 1200 MPa view details
Tensile Strength 1300 MPa view details
Elongation, A 4 % view details
Reduction of Area val1
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% view details
Yield Strength, Rp0.2 174 ksi view details
Tensile Strength 188.5 ksi view details
Elongation, A 4 % view details
Reduction of Area val1
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% view details

Physical Properties

Temperature

0 - 30°C
PROPERTY / VALUE
Modulus of Elasticity 80 — 130 GPa view details
Density 4.3 — 5.1 kg/dm³ view details
Modulus of Elasticity 11.6 E+03 — 18.9 E+03 ksi view details
Density 0.155 — 0.184 lb/in³ view details

Composition

CRITERIA
VALUE
UNIT
CAS NUMBER
CRITERIA
Al
VALUE
4.4000 – 5.7000
UNIT
%
CAS NUMBER
7429-90-5
CRITERIA
C
VALUE
≤ 0.1000
UNIT
%
CAS NUMBER
7440-44-0
CRITERIA
Cr
VALUE
2.5000 – 3.5000
UNIT
%
CAS NUMBER
7440-47-3
CRITERIA
Fe
VALUE
val1
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UNIT
%
CAS NUMBER
7439-89-6
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
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
CRITERIA
V
VALUE
val1
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UNIT
%
CAS NUMBER
7440-62-2
CRITERIA
Y
VALUE
val1
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UNIT
%
CAS NUMBER
7440-65-5

EN 4675: 2011 / Aerospace series - Titanium Ti-P63002 (Ti5Al5Mo5V3Cr0.4Fe) - Rm ≥ 1 300 MPa - Bars - De < 110 mm

Heat Treatments

  • 15°C to 40°C below beta-transus/ t=1h/ AC or inert gas + 540°C <= &theta; <= 650°C / t >= 8h /AC