The Ir_xRe_1−x (0.1≤ x ≤0.7) alloys are hexagonal structured inclusion material used in an on-orbit communication satellite. The characteristic features of high-temperature alloys Ir_xRe_1−x (0.1≤ x ≤0.7) are investigated by the theoretical evaluation of thermophysical and ultrasonic properties at room temperature. Initially, higher-order elastic constants of the alloys are calculated using the simple interaction potential model approach. With the help of this other elastic moduli, elastic stiffness constants and hardness parameters are estimated at room temperature for elastic and mechanical characterization. Later on, the ultrasonic velocity and thermal relaxation time of chosen alloys are evaluated utilizing calculated values of SOECs and lattice parameters within the same physical conditions. The orientation-dependent ultrasonic velocities and thermal relaxation time have been also evaluated for the determination of anisotropic behaviour and thermophysical properties. The obtained results are analysed to explore the inherent properties of Ir_xRe_1−x alloys.

Ir _x Re _1-x（0.1≤x≤0.7）合金是在轨通信卫星中使用的六方结构夹杂物。高温合金Ir _x Re _1-x的特征（0.1≤x≤0.7）通过在室温下的热物理和超声性能的理论评估进行研究。最初，使用简单的相互作用势模型方法计算合金的高阶弹性常数。借助此其他弹性模量，可以在室温下估算弹性刚度常数和硬度参数，以进行弹性和机械表征。随后，在相同的物理条件下，利用SOEC的计算值和晶格参数评估所选合金的超声速度和热弛豫时间。还对取向相关的超声速度和热弛豫时间进行了评估，以确定各向异性行为和热物理性质。_x Re _1-x合金。