主动冷却陶瓷基复合材料结构技术是一种新型热防护技术,它综合了耐高温材料与冷却结构各自优势,可显著提高构件热容限,降低单位质量,提高推重比,在超燃冲压发动机等先进推进系统上具有良好应用潜力,被认为是实现低成本、高可靠空间飞行的关键技术之一,得到美、法、德等国的积极研究,基于前期机理探讨及缩比件考核结果,目前正向全尺寸工程样机阶段过渡.其中,利用多种精细成型工艺在纤维增强陶瓷基复合材料(CMC)构件内部成型再生冷却流道或发汗冷却多孔结构的全CMC方案具有较高的先进性与可行性,代表了未来发展方向.
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