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Design, Analysis and Testing of a Novel Deployable Telescope for Earth Observation using Small Satellites

机译:使用小卫星进行地球观察的新型展开望远镜的设计,分析和测试

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The Surrey Space Centre (SSC) and Surrey Satellite Technology Ltd (SSTL) have collaborated in a Centre for Earth Observation Instrumentation (CEOI) sponsored project to design a deployable Cassegrain telescope. Deployable structures have proved very successful in the past decades for deployment of sensors and solar panels, to name a few. Therefore, attention has naturally turned to incorporating deployable structures into more complex space systems. Optical telescopes are currently flown with a fixed focal length, set by the desired magnification, which limits their use to larger satellites. Incorporating a deployable system, to extend to the fixed length from a smaller volume, could open the door for smaller satellites to carry larger optical telescopes, making Earth observation more accessible for research and businesses. The aim of this project was to increase the capability of small satellites for Earth observation by demonstrating a proof of concept breadboard and development model of a deployable Cassegrain telescope. The design uses three concentric carbon fibre barrels deployed into lockout stops by three leadscrew sets equi-spaced around the barrels. This paper will provide an overview of the design, analysis and test campaign for this deployable optical system. Demonstration and validation of the design was completed on two fronts, analysis and test. The requirements can be simplified to deployment repeatability, structural performance and thermal stability. The deployment repeatability was physically tested using an aluminium test rig and suspended digital test indicators. The structural performance was first modelled using finite element (FE) software then experimentally using a suspended mini-shaker. Finally, the thermal stability of the system was investigated using FE and validated experimentally, using an autocollimator, reference tube and thermal chamber. The deployment results for both the development model show that the system can reliably deploy
机译:Surrey Space Center(SSC)和萨里卫星科技有限公司(SSTL)在地球观测仪器(CEOI)的中心合作,赞助项目,以设计一个可展开的Cassegrain望远镜。在过去的几十年里,可部署的结构已经证明是非常成功的传感器和太阳能电池板的部署,以命名几十年。因此,注意力自然地转向将可部署的结构融入更复杂的空间系统。光学望远镜目前用固定的焦距飞行,由所需的倍率设定,限制其对较大卫星的用途。结合可部署的系统,延伸到从较小的体积延伸到固定长度,可以为较小的卫星打开门以携带较大的光学望远镜,使地球观察更容易获得研究和企业。该项目的目的是通过展示可展示的Cassegrain望远镜的概念面包板和开发模型的证据来提高地球观测的小卫星的能力。该设计使用朝向锁定锁定的三个同心碳纤维桶通过三个铅螺丝套在桶周围平等。本文将概述该可部署光学系统的设计,分析和测试活动。在两个前面,分析和测试方面完成了设计的示范和验证。可以简化要求以展开可重复性,结构性能和热稳定性。使用铝制试验台和悬挂的数字测试指示器进行物理测试部署重复性。第一次使用有限元(FE)软件进行结构性能,然后使用悬浮的迷你振动器进行实验。最后,使用Fe和实验验证系统的热稳定性,使用自动调用器,参考管和热室进行实验验证。两个开发模型的部署结果表明系统可以可靠地部署

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