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DESIGN AND DEVELOPMENT OF CFRP TUBULAR STRUCTURE FOR SOFT X-RAY TELESCOPE PAYLOAD OF ASTROSAT

机译:雾化物软X射线望远镜有效性的CFRP管状结构的设计与开发

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摘要

India has launched an astronomical space based observatory ASTROSAT in the year 2015 for unravelling the some of the secrets of our universe. Soft X-ray Telescope (SXT) was one among the payloads onboard for studying the sources of Soft X-rays in deep space. A composite structure was required for this purpose. It had to support the pay load elements and maintain their relative locations precisely during launch as well as during its operation, in-orbit. The interface with the spacecraft was at the middle of the SXT structure with one part is inside and remaining part is outside of the spacecraft deck. The structural design was carried out to meet all the structural design requirements such as stability, stiffness and strength with minimum mass under the constraints of spacecraft interface and envelope. This paper presents the details of the structural design, development and qualification of a CFRP tubular SXT structure, which has been functioning satisfactorily in-orbit.
机译:印度在2015年推出了一个天文空间的天文架,用于解开我们宇宙的一些秘密。 软X射线望远镜(SXT)是船上有效载荷中的一个,用于研究深空中软X射线的来源。 为此目的需要复合结构。 它必须支持支付负载元素,并在发布期间保持相对位置以及在其运行过程中,在轨道上。 与航天器的界面在SXT结构的中间,一个部分是内部,剩余部分位于航天器甲板的外部。 进行了结构设计,以满足所有结构设计要求,如稳定性,刚度和强度,在航天器界面和包络的约束下具有最小质量。 本文介绍了CFRP管状SXT结构的结构设计,开发和资格的细节,该结构一直在轨道令人满意地运作。

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