Ti5Al5Mo5V3Cr0.4Fe (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:
-
Mechanical Properties
Temperature
Physical Properties
Temperature
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
Full data access requires a free trial.
Sign Up Free
UNIT
%
CAS NUMBER
7439-89-6
CRITERIA
Mo
VALUE
val1
Full data access requires a free trial.
Sign Up Free
UNIT
%
CAS NUMBER
7439-98-7
CRITERIA
N
VALUE
val1
Full data access requires a free trial.
Sign Up Free
UNIT
%
CAS NUMBER
7727-37-9; 17778-88-0
CRITERIA
O
VALUE
val1
Full data access requires a free trial.
Sign Up Free
UNIT
%
CAS NUMBER
7782-44-7; 17778-80-2
CRITERIA
Other each
VALUE
val1
Full data access requires a free trial.
Sign Up Free
UNIT
%
CAS NUMBER
CRITERIA
Other total
VALUE
val1
Full data access requires a free trial.
Sign Up Free
UNIT
%
CAS NUMBER
CRITERIA
Ti
VALUE
val1
Full data access requires a free trial.
Sign Up Free
UNIT
%
CAS NUMBER
7440-32-6
CRITERIA
V
VALUE
val1
Full data access requires a free trial.
Sign Up Free
UNIT
%
CAS NUMBER
7440-62-2
CRITERIA
Y
VALUE
val1
Full data access requires a free trial.
Sign Up Free
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 <= θ <= 650°C / t >= 8h /AC
-
39 Cross References
-
12 Composition
-
12 Mechanical Properties
-
2 Physical Properties
-
1 Heat Treatment
-
- Metallography
-
- Machinability
-
- Stress-Strain
-
- Formability
-
- Fatigue
-
- Fracture
-
- Creep
-
- Joints
-
- Coatings
-
- Dimensions
-
- Tribology
-
4283 Corrosion
-
- Ageing
-
- Weatherability
-
- Irradiation
-
- Total Suppliers