About Mo-25 Re Alloy
Molybdenum and rhenium are both refractory metals. These metals are well known for their extraordinary resistance to heat and wear. Key requirement to withstand high temperatures is a high melting point and stable mechanical properties (e.g. high hardness) even at high temperatures. These metals are usually combined together to obtain desired fabricability, thermal and mechanical properties. The molybdenum-rhenium alloys exhibiting good low-temperature ductility. The Mo-35Re alloy also has a low ductile-to-brittle transition temperature in the as-cast condition. The alloy is extremely difficult to fracture by hammering as-cast material at temperatures down to -196°C.
|Name||Mo-25 Re Alloy|
|Phase at STP||solid|
|Ultimate Tensile Strength||1100 MPa|
|Young’s Modulus of Elasticity||360 GPa|
|Brinell Hardness||350 BHN|
|Melting Point||2527 °C|
|Thermal Conductivity||70 W/mK|
|Heat Capacity||220 J/g K|
Composition of Mo-25 Re Alloy
Molybdenum-rhenium alloys containing up to 40% rhenium are predominantly single-phase body-centered cubic solid-solution alloys.
Applications of Mo-25 Re Alloy
Rhenium is considered highly desirable as an alloying addition with other refractory metals. Molybdenum-rhenium alloys offer high temperature strength; the combination drastically increases ductility and tensile strength. Rhenium is gaining acceptance in nuclear reactors, rockets, and other commercial and aerospace applications.
Mechanical Properties of Mo-25 Re Alloy
Strength of Mo-25 Re Alloy
In mechanics of materials, the strength of a material is its ability to withstand an applied load without failure or plastic deformation. Strength of materials basically considers the relationship between the external loads applied to a material and the resulting deformation or change in material dimensions. In designing structures and machines, it is important to consider these factors, in order that the material selected will have adequate strength to resist applied loads or forces and retain its original shape.
Strength of a material is its ability to withstand this applied load without failure or plastic deformation. For tensile stress, the capacity of a material or structure to withstand loads tending to elongate is known as ultimate tensile strength (UTS). Yield strength or yield stress is the material property defined as the stress at which a material begins to deform plastically whereas yield point is the point where nonlinear (elastic + plastic) deformation begins. In case of tensional stress of a uniform bar (stress-strain curve), the Hooke’s law describes behaviour of a bar in the elastic region. The Young’s modulus of elasticity is the elastic modulus for tensile and compressive stress in the linear elasticity regime of a uniaxial deformation and is usually assessed by tensile tests.
See also: Strength of Materials
Ultimate Tensile Strength of Mo-25 Re Alloy
Ultimate tensile strength of Mo-25 Re Alloy is 1100 MPa.
Yield Strength of Mo-25 Re Alloy
Yield strength of Mo-25 Re Alloy is N/A.
Modulus of Elasticity of Mo-25 Re Alloy
The Young’s modulus of elasticity of Mo-25 Re Alloy is 360 GPa.
Hardness of Mo-25 Re Alloy
In materials science, hardness is the ability to withstand surface indentation (localized plastic deformation) and scratching. Brinell hardness test is one of indentation hardness tests, that has been developed for hardness testing. In Brinell tests, a hard, spherical indenter is forced under a specific load into the surface of the metal to be tested.
The Brinell hardness number (HB) is the load divided by the surface area of the indentation. The diameter of the impression is measured with a microscope with a superimposed scale. The Brinell hardness number is computed from the equation:
Brinell hardness of Mo-25 Re Alloy is approximately 350 BHN (converted).
See also: Hardness of Materials
Thermal Properties of Mo-25 Re Alloy
Mo-25 Re Alloy – Melting Point
Melting point of Mo-25 Re Alloy is 2527 °C.
Note that, these points are associated with the standard atmospheric pressure. In general, melting is a phase change of a substance from the solid to the liquid phase. The melting point of a substance is the temperature at which this phase change occurs. The melting point also defines a condition in which the solid and liquid can exist in equilibrium. For various chemical compounds and alloys, it is difficult to define the melting point, since they are usually a mixture of various chemical elements.
Mo-25 Re Alloy – Thermal Conductivity
Thermal conductivity of Mo-25 Re Alloy is 70 W/(m·K).
The heat transfer characteristics of a solid material are measured by a property called the thermal conductivity, k (or λ), measured in W/m.K. It is a measure of a substance’s ability to transfer heat through a material by conduction. Note that Fourier’s law applies for all matter, regardless of its state (solid, liquid, or gas), therefore, it is also defined for liquids and gases.
The thermal conductivity of most liquids and solids varies with temperature. For vapors, it also depends upon pressure. In general:
Most materials are very nearly homogeneous, therefore we can usually write k = k (T). Similar definitions are associated with thermal conductivities in the y- and z-directions (ky, kz), but for an isotropic material the thermal conductivity is independent of the direction of transfer, kx = ky = kz = k.
Mo-25 Re Alloy – Specific Heat
Specific heat of Mo-25 Re Alloy is 220 J/g K.
Specific heat, or specific heat capacity, is a property related to internal energy that is very important in thermodynamics. The intensive properties cv and cp are defined for pure, simple compressible substances as partial derivatives of the internal energy u(T, v) and enthalpy h(T, p), respectively:
where the subscripts v and p denote the variables held fixed during differentiation. The properties cv and cp are referred to as specific heats (or heat capacities) because under certain special conditions they relate the temperature change of a system to the amount of energy added by heat transfer. Their SI units are J/kg K or J/mol K.
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