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Thermal Protections Systems : Heritage - Development Status - Perspectives

机译:热保护系统:遗产-发展现状-观点

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Ceramic Matrix Composite (CMC) TPS belong to the group of key technologies that will enable the flight of hypersonic and re-entry vehicles, as they provide a high temperature resistant non ablative outer mould line for enhanced aerodynamic control. These thermo-structural composites have been developed in Herakles, Safran group for more than 20 years, and have reached a high Technology Readiness Level. Their maturity can now only be improved through an actual flight, which will precisely be made through the current development, manufacturing, and soon to be launched Intermediate experimental Vehicle (IXV). The IXV, atmospheric re-entry demonstrator developed within the FLPP (Future Launcher Preparatory Program) and funded by ESA, aims at developing a demonstration vehicle that will give Europe a unique opportunity to increase its know-how in the field of advanced atmospheric re-entry technologies. A key technology that will be demonstrated in real conditions through the flight of this ambitious vehicle is the CMC-based Thermal Protection System (TPS) that is the current baseline for the thermal protection of the windward area, as well as the nose assembly. The development of the IXV vehicle, has gained considerable momentum since the beginning of 2010 with the start of the detailed design phase that has been concluded in early 2011, and with the start of the qualification and flight hardware manufacturing phase. The detailed design phase comprised extensive thermal and thermo-mechanical analyses, small-scale tests on the various components of the Windward and Nose Assemblies, and large scale prototypes manufacturing. Among those tests, some have specifically made to assess the behavior of the TPS during re-entry The paper will describe the important TPS heritage available at Herakles, Safran group, the current technological achievements of the development of the Windward Assembly TPS and Nose Assembly, and the activities that are initiated and planned for the qualification and the delivery of the flight hardware. It will also present future perspectives and potential applications..
机译:陶瓷基复合材料(CMC)TPS属于使高超音速和重入飞行器飞行的关键技术,因为它们提供了耐高温的非烧蚀外模线以增强空气动力学控制。这些热结构复合材料已经在赛峰集团的Herakles开发了20多年,并且达到了很高的技术准备水平。现在只能通过实际飞行来提高它们的成熟度,这将通过当前的开发,制造以及即将推出的中间实验车(IXV)来精确地实现。 IXV是在FLPP(未来发射器预备计划)中开发并由ESA资助的大气再进入演示器,旨在开发一种演示工具,这将为欧洲提供一个独特的机会,以增加其在先进大气再利用领域的专业知识入门技术。通过这种雄心勃勃的飞行器在实际条件下将展示的一项关键技术是基于CMC的热保护系统(TPS),它是迎风区域以及机头组件的当前热保护的当前基准。自2010年初以来,IXV车辆的开发获得了可观的动力,该阶段的详细设计阶段已于2011年初结束,而鉴定和飞行硬件制造阶段也已开始。详细的设计阶段包括广泛的热和热机械分析,对迎风和鼻子组件的各个组件的小规模测试以及大规模的原型制造。在这些测试中,有一些是专门用来评估TPS在重返过程中的行为的。本文将介绍赛峰集团Herakles拥有的重要TPS传统,Windward Assembly TPS和Nose Assembly开发的最新技术成就,以及为鉴定和交付飞行硬件而启动和计划的活动。它还将介绍未来的观点和潜在的应用。

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