ON THE APPLICATION OF FUNCTIONAL APPROACH TO CREATING AND PROVIDING OPERATIONAL CHARACTERISTICS OF ULTRALIGHT THERMAL PROTECTION OF REUSABLE LAUNCH SPACECRAFT
The main task of the research is to establish the regularities of the formation of a non-detachable compound of thin-walled elements from the Ni-20Cr-6Al-1Ti-1Y2O3 alloy and to determine the functional condition of the influence of soldering modes on the physical-mechanical characteristics of the compound. It has been shown the modeling of temperature fields in ANSYS 18.1. It has been established that the process of vacuum soldering should take place at a temperature of 1350°C for 15-20 min; the strength of the resulting compound is 390-420 MPa when the sample is stretched. The obtained information can be used as a theoretical basis for the development of the manufacturing process of the elements of the spaceship heat-shielding system.