航空航天
陶瓷
结构材料
材料科学
使用寿命
氧化物
机械工程
热的
环境科学
熔化温度
核工程
比例(比率)
工艺工程
航空航天工程
法律工程学
高压
结构完整性
磁导率
碳化物
脆弱性
复合材料
熔点
服务(商务)
最高温度
透视图(图形)
航天飞机热防护系统
大气压力
作者
Fei Li,Guojun Zhang,Yanchun Zhou,Xinghong Zhang
标识
DOI:10.26599/jac.2025.9221231
摘要
Aerodynamic heating, oxidation, ablation, and high dynamic pressure represent the extreme environments that aerospace vehicles must withstand during high-Mach atmospheric or trans-atmospheric flight. The temperature of critical components on the vehicles can reach 3000 °C or higher. Such extreme environment imposes stringent requirements on thermal protection materials, such as ultra-high temperature ceramics (UHTCs) and their composites. It has come to light that the formation of a dense oxide scale with low oxygen permeability is crucial for ensuring the ablation resistance of UHTCs. As such, searching for oxides with melting points exceeding 3000 °C is one of the emerging directions. This perspective aims to briefly review the development of UHTCs and their composites over the past few decades. In addition, promising directions are proposed to meet the extreme environments. Concurrently, the assistance of multiscale modeling techniques to accelerate the development and application of UHTCs and their composites is emphasized.
科研通智能强力驱动
Strongly Powered by AbleSci AI