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NEW PLASMA SPRAYED CERAMIC COATINGS TECHNIQUES. APPLICATION TO SPACE.

机译:新的等离子喷涂陶瓷涂层技术。应用于空间。

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The purpose of this paper is to present on one hand the applicability of fiber-reinforced Ultra High Temperature Ceramics (UHTC) and UHTC coated metals to space missions and on the other hand the plasma sprayed ceramic coating technique on refractory metals for space applications. CIRA has designed two UHTC winglets to be installed on the Australian rocket SCRAMSPACE. The paper describes the new material selected for this experiment, a fiber reinforced UHTC, and a new technology of UHTC coating. The present paper presents also, an application of ceramic coatings technique in the field of aerospace hypersonic vehicles, where the high thermal loads are coupled with highly reactive plasma environment. The results of a material selection campaign conducted by CSM and CIRA is presented. A set of substrates, coatings and deposition techniques have been individuated as possible candidates for a real flight test. Many samples have been realized and tested. A first selection was based on pull test, the final selection was accomplished by means of plasma torch test, exposing conical samples to very high temperatures. The result is at the selection of a substrate/coating system that shall be used in future real flight applications.
机译:本文的目的是一方面介绍纤维增强的超高温陶瓷(UHTC)和UHTC涂层金属在太空任务中的适用性,另一方面,等离子喷涂陶瓷涂层技术在用于太空应用的难熔金属上的适用性。 CIRA设计了两个将在澳大利亚火箭SCRAMSPACE上安装的UHTC小翼。本文介绍了为此实验选择的新材料,纤维增强UHTC和UHTC涂层的新技术。本文还介绍了陶瓷涂层技术在航空高超声速飞行器领域中的应用,在该领域中,高热负荷与高反应性等离子体环境相结合。介绍了CSM和CIRA进行的材料选择运动的结果。一组基材,涂层和沉积技术已被单独选作实际飞行测试的可能候选者。已经实现并测试了许多样本。第一次选择是基于拉力试验,最终选择是通过等离子炬试验完成的,将锥形样品暴露在非常高的温度下。结果就是选择了在将来的实际飞行应用中应使用的基材/涂层系统。

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