一种热平衡等温机制的新型热防护及相关技术

给出了一种适用于高超声速飞行器热防护的新概念——疏导式热防护，其基本理论是利用热平衡等温机制，使防热层趋于一等温体，实现热负载平衡。针对这一概念，进行了较为系统的研究，包括原理、分析方法、实现疏导式热防护的关键技术。研究结果表明，疏导式热防护技术可有效地减少高热流区的温度和热应力，是一种有效的非烧蚀热防护技术。

A New Thermal Protection Technology Based on Heat BalanceIsothermal Mechanism

This paper provides a new thermal protection method, heat balance thermal protection, which is adaptable for thermal protection of hypersonic vehicle. Its principal theory is thermal equilibrium isothermal mechanism. By using heat balance thermal protection the temperature of thermal protection layer turns into equality. Systematic research has been done directly about heat balance thermal protection, including principle, analytical methods of the theory and key techniques. It is shown that the temperature and heat stress can be cut down effectively by the heat balance thermal protection. The heat balance thermal protection is effective in non ablating thermal protection of hypersonic vehicle.