Single-side high-temperature testing device of hypersonic aircraft material in 1800-degree aerobic environment

Abstract

The invention discloses a single-side high-temperature testing device of a hypersonic aircraft material in an 1800-degree aerobic environment. The testing device comprises a silicon-molybdenum heater array, a high-temperature ceramic support, a heat insulation base, a high-temperature ceramic flat plate, a hypersonic aircraft plane testing part material, a high-temperature heat insulation material, a thermocouple temperature sensor and a computer. According to the device, when a radiation heating experimental research of the hypersonic aircraft material is conducted, a single-side flight thermal environment for a high-mach number aircraft in an aerobic environment is achieved, heat insulation characteristic parameters of the hypersonic aircraft material in an extreme, aerobic and high-temperature environment are measured, and important extreme thermal environment testing methods are provided for high-speed spacecraft and aircraft production.

Description

technical field [0001] The invention relates to a high-temperature test device for a single side of a hypersonic aircraft material in an aerobic environment of 1800 degrees. Especially when simulating the radiation heating of high Mach number missile flight tests, it can reproduce the thermal environment of the one-sided flight of hypersonic vehicles under real aerobic conditions, and obtain the heat insulation characteristics of hypersonic vehicle materials in extreme oxidizing high-temperature environments, etc. performance parameters. It provides important thermal test means for the development of high-speed aerospace vehicles. Background technique [0002] Because hypersonic vehicles can achieve global long-distance and rapid arrival, implement effective high-altitude, high-speed penetration and fast and precise strikes, they have extremely important application value and strategic significance. Hypersonic vehicles have become a research hotspot among major aerospace po...

AI Technical Summary

Problems solved by technology

In the above-mentioned one-sided thermal test, the heat-resistant material and the heat-resistant structure test piece need to have a difference between the hot surface and the cold surface, so the heat-resistant material and the heat-resistant structure cannot be heated in a high-temperature heating furnace as a whole.

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