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Communication Architecture and Operation Strategies for the electrically propelled CubeSat and re-entry Capsule System CAPE

机译:电气推进立方体和重新入口胶囊系统斗篷的通信架构和操作策略

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The range of applications supported by CubeSats has evolved. Multiple technologies converged due to improvements in micro-systems, communications and sensing. A breakthrough of propulsion technologies and nanoscale satellite applications is imminent, and all of them are enabling an increase of mission flexibility and novel ways of conducting science, while providing a cost-effective platform. CAPE, the CubeSat Atmospheric Probe for Education, is a 2U-CubeSat platform for testing a novel electric-propulsion system in low earth orbit, which carries the smallest deployable miniature re-entry capsule. The Service and Deorbit module is equipped with a pulsed plasma-thruster (PPT) for orbit and re-entry control, developed by the Institute of Space Systems of the University of Stuttgart (IRS). Due to the resulting demise this mission will not produce space debris. This mission is a first of its kind as the re-entry capsule is an autonomous system with dedicated communication equipment active during re-entry and the service and de-orbit module with an own comsystem that will transmit housekeeping and e-thruster performance characteristics. For achieving this a new communication architecture is required serving the needs of a standard CubeSat with respect to TMTC. The mission design drivers are the PPT PETRUS and the capsule itself. The thruster will successively adjust CAPE's orbit. Permanent tracking is required to validate thruster effectivity and maintain the com-link. Furthermore the plasma will be an interference source to the communication system during re-entry. The communication architecture shall be robust against these effects. The capsule has its own communication system for transmitting scientific data while travelling through the atmosphere. The driving requirement is the data completeness of both systems. The study provides selection criteria of the different frequency bands, the properties of the communication system onboard, the ground segment infrastructure
机译:CubeSats支持的应用范围已进化。多种技术因微系统,通信和传感的改进而融合。推进技术和纳米级卫星应用的突破即将来临,所有这些都可以增加任务灵活性和新颖的进行科学方式,同时提供具有成本效益的平台。 Cape Cape,CubeSat大气探测为教育,是一个2U立方体平台,用于测试低地轨道中的新型电动推进系统,携带最小的可展开的微型再进入胶囊。该服务和防床模块配备了由Stuttgart大学的空间系统(IRS)的空间系统开发的轨道和重新进入控制的脉冲等离子体推进器(PPT)。由于产生的消亡,这项任务不会产生空间碎片。这项任务是第一类,因为重新进入胶囊是一个自治系统,具有专用通信设备在重新入境和服务和去轨模块期间具有自己的ComSystem,它将传输家务和电子推进器性能特征。为了实现这一新的通信架构,需要在TMTC方面提供标准CubeSAT的需求。任务设计司机是PPT Petrus和胶囊本身。推进器将连续调整Cape的轨道。需要永久跟踪以验证推进器效率并维护COM-LINK。此外,在重新进入期间,等离子体将是通信系统的干扰源。通信架构应对这些效果稳健。胶囊具有自己的通信系统,用于在通过大气行驶时传输科学数据。驾驶要求是两个系统的数据完整性。该研究提供了不同频带的选择标准,通信系统的性质,地板,地面段基础架构

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