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Master Bond adhesives

TIMET 75A CP Titanium (ASTM Grade 4)
Categories: Metal; Nonferrous Metal; Titanium Alloy; Unalloyed/Modified Titanium

Material Notes: Commercially Pure Titanium.

Industry Specifications: USA Aerospace: AMS 4901. Germany Engineering: 3.7065. Germany Aerospace: 3.7064. France: T-60. UK Aerospace Specification BS TA. 6.

Features: The mechanical properties of CP titanium are influenced by small additions of oxygen and iron. By careful control of these additions, the various grades of commercially pure titanium are produced to give properties suited to different applications. TIMETAL 75A is equivalent to ASTM Grade 4. It has the highest strength of the four ASTM commercially pure titanium grades in addition to good ductility and moderate formability. The benefits of the good strength to weight ratio of TIMETAL 75A are retained at moderate temperatures. It has good impact properties at low temperatures. It can be satisfactorily welded, machined, cold worked, hot worked, and cast. It is nonmagnetic.

Typical heat treatment for this alloy: Anneal at 700°C for 1 hour and air cool. Stress Relieve at 500°C for 30 mins and air cool.

Data provided by TIMET.

Key Words: UNS R50700
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Physical PropertiesMetricEnglishComments
Density 4.51 g/cc0.163 lb/in³Typical
 
Mechanical PropertiesMetricEnglishComments
Tensile Strength, Ultimate 680 MPa98600 psiTypical
 209 MPa
@Temperature 450 °C
30300 psi
@Temperature 842 °F
 227 MPa
@Temperature 400 °C
32900 psi
@Temperature 752 °F
 284 MPa
@Temperature 300 °C
41200 psi
@Temperature 572 °F
 381 MPa
@Temperature 200 °C
55300 psi
@Temperature 392 °F
 537 MPa
@Temperature 100 °C
77900 psi
@Temperature 212 °F
Tensile Strength, Yield 560 MPa
@Strain 0.2 %
81200 psi
@Strain 0.2 %
Typical
 92.0 MPa
@Strain 0.2 %,
Temperature 450 °C
13300 psi
@Strain 0.2 %,
Temperature 842 °F
 101 MPa
@Strain 0.2 %,
Temperature 400 °C
14600 psi
@Strain 0.2 %,
Temperature 752 °F
 149 MPa
@Strain 0.2 %,
Temperature 300 °C
21600 psi
@Strain 0.2 %,
Temperature 572 °F
 231 MPa
@Strain 0.2 %,
Temperature 200 °C
33500 psi
@Strain 0.2 %,
Temperature 392 °F
 364 MPa
@Strain 0.2 %,
Temperature 100 °C
52800 psi
@Strain 0.2 %,
Temperature 212 °F
Elongation at Break 23 %23 %Typical
 27 %
@Temperature 100 °C
27 %
@Temperature 212 °F
 33 %
@Temperature 200 °C
33 %
@Temperature 392 °F
 33 %
@Temperature 400 °C
33 %
@Temperature 752 °F
 35 %
@Temperature 300 °C
35 %
@Temperature 572 °F
Reduction of Area 46 %46 %Typical
Modulus of Elasticity 105 - 120 GPa15200 - 17400 ksiTypical
Fatigue Strength 376 MPa
@# of Cycles 1.00e+7
54500 psi
@# of Cycles 1.00e+7
Smooth, Kt = 1. Fatigue ratio = 0.56
Bend Radius, Minimum 3.0 t
@Thickness 2.00 mm
3.0 t
@Thickness 0.0787 in
Typical; sheet
 
Electrical PropertiesMetricEnglishComments
Electrical Resistivity 0.0000600 ohm-cm0.0000600 ohm-cm
 
Thermal PropertiesMetricEnglishComments
CTE, linear  8.60 µm/m-°C
@Temperature 20.0 - 100 °C
4.78 µin/in-°F
@Temperature 68.0 - 212 °F
 9.50 µm/m-°C
@Temperature 20.0 - 300 °C
5.28 µin/in-°F
@Temperature 68.0 - 572 °F
 9.70 µm/m-°C
@Temperature 20.0 - 425 °C
5.39 µin/in-°F
@Temperature 68.0 - 797 °F
Thermal Conductivity 16.95 W/m-K117.6 BTU-in/hr-ft²-°F
Maximum Service Temperature, Air 425 °C797 °FContinuous
 540 °C1000 °FIntermittent
Beta Transus 950 °C1740 °F
 
Component Elements PropertiesMetricEnglishComments
Carbon, C <= 0.080 %<= 0.080 %
Hydrogen, H <= 0.015 %<= 0.015 %
Iron, Fe <= 0.50 %<= 0.50 %
Nitrogen, N <= 0.050 %<= 0.050 %
Oxygen, O <= 0.40 %<= 0.40 %
Titanium, Ti >= 98.6 %>= 98.6 %Calculated as remainder

Some of the values displayed above may have been converted from their original units and/or rounded in order to display the information in a consistent format. Users requiring more precise data for scientific or engineering calculations can click on the property value to see the original value as well as raw conversions to equivalent units. We advise that you only use the original value or one of its raw conversions in your calculations to minimize rounding error. We also ask that you refer to MatWeb's terms of use regarding this information. Click here to view all the property values for this datasheet as they were originally entered into MatWeb.

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