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Solid-fuel Rocket Engines: Layered Composite Materials Manufacturing and Thermal Diffusivity Measurements

机译:固体燃料火箭发动机:多层复合材料制造和热扩散率测量

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This communication presents thermal diffusivity measurements of fourteen layered insulating composite materials. Composite materials that were taken under investigation contained matrixes based on epoxy and phenol-formaldehyde resins and reinforcements, such as glass, basalt fiber and wrapping or ceramic paper. They were all prepared by the Rocket Section of the Students Space Association (RS-SSA). Manufacturing process of samples is described. Additional objective of this research was to obtain the quality of such prepared materials and if they are reliable enough to be used in solid-fuel rocket motors. Use of composite materials to build combustion chamber walls of solid fuel rocket engines, rather than metal, leads to weight reduction and increases amount of fuel that rocket can carry. That improves performances and gives new possibilities for rocket applications. To apply new high performance solid fuels, development of new composite materials was required. Analysis of thermal properties gives the answer, which material should be used for new solid-fuel rockets designed by RS-SSA.
机译:此通信显示了十四个层状绝缘复合材料的热扩散率测量值。接受调查的复合材料包含基于环氧树脂和酚醛树脂的基质以及增强材料,例如玻璃,玄武岩纤维和包装纸或陶瓷纸。它们都是由学生空间协会(RS-SSA)的火箭处准备的。描述了样品的制造过程。这项研究的另一个目的是获得这种准备好的材料的质量,以及它们是否足够可靠以用于固体燃料火箭发动机。使用复合材料而不是金属来建造固体燃料火箭发动机的燃烧室壁,可以减轻重量并增加火箭可以携带的燃料量。这提高了性能,并为火箭应用提供了新的可能性。为了使用新的高性能固体燃料,需要开发新的复合材料。热性能分析给出了答案,哪种材料应用于RS-SSA设计的新型固体燃料火箭。

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