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德国空间技术规划局(未来空间运输系统技术 )通过研究开发出全陶瓷体襟翼 (BF)。BF适用于美国NASA的X 38飞行器V 2 0 1,X 38BF被称为负荷运行的“热结构” ,它被设计成为全陶瓷结构 ,这样它就不再需要附加的热防护 ,因此可以减轻系统质量。BF完全由C/SiC陶瓷基复合材料制成 ,以便能够在温度超过 180 0℃和机械载荷高达 5 0kN的条件下进行操作。最后对陶瓷基复合材料(CMC)及其发展作了详细介绍。
The German Space Technology Planning Agency (Future Space Transport Systems Technology) has developed all-ceramic body flaps (BF) through research. BF For X 38 aircraft NASA USA V 2 0 1 The X 38BF, known as a “thermal structure” for load operation, is designed as an all-ceramic structure so that it no longer requires additional thermal protection and therefore reduces the system effort quality. BF is entirely made of C / SiC ceramic matrix composites to operate at temperatures in excess of 180 ° C and mechanical loads up to 50 kN. Finally, the ceramic matrix composites (CMC) and its development are described in detail.