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DELTA-SAT: THE CONCURRENT PRE-PHASE A DESIGN OF A THERMOSPHERIC EXPLORATION MICROSATELLITE

机译:DELTA-SAT:同时进行热勘探微卫星的设计

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The ‘Microsatellite Engineering' Master course at the Faculty of Aerospace Engineering of the Delft Universityof Technology aims to bridge the gap between education and professional engineering practise by using a projectbasedapproach to space systems engineering education. The course comprised of a mission and microsatellite designproject, using collaborative engineering methodologies to achieve the design of a thermospheric explorationmicrosatellite. This paper details design process and resulting technical design of this microsatellite, ‘DELTA-Sat'.The project work entailed the simultaneous conceptual design of the physical and functional architecture of amicrosatellite. Emphasis was placed on payload requirements and engineering of the spacecraft bus functionalities,with design activities occurring within a rigorous systems engineering framework. Further work also addressedoverall mission design to support the development and operations of DELTA-Sat.The technical result of the DELTA-Sat exercise was the preliminary stage (Phase 0/Pre-Phase A) design of amicrosatellite and supporting mission architecture as a result of subsystem trade-offs. Subsystem designs weredefined for payload, propulsion, attitude determination and control system (ADCS), structural, thermal,communication, electrical power system (EPS), and command and data handling system (CDHS) aspects of thespacecraft. Additionally, mass and power budgets, a launch segment, and a life cycle cost estimation were alsodefined. The resulting system makes innovative use of drag-free technology to undertake measurements in the lowerthermosphere, while enjoying the advantages of reduced cost and development time offered by microsatellites. Inconclusion, the DELTA-Sat project allowed students to gain valuable experience in systems engineeringmethodologies by designing a novel microsatellite mission. The resulting DELTA-Sat design benefits from increasedsensitivity to subsystem interdependency and customer requirements, resulting from the collaborative nature of thedesign process.
机译:代尔夫特大学航空工程学院的“微卫星工程”硕士课程 技术学院旨在通过使用基于项目的项目来弥合教育与专业工程实践之间的鸿沟 空间系统工程教育方法。该课程包括任务和微卫星设计 该项目,使用协作工程方法来实现热层勘探的设计 微卫星。本文详细介绍了这种“ DELTA-Sat”微卫星的设计过程以及由此产生的技术设计。 该项目的工作需要同时进行物理和功能体系结构的概念设计。 微卫星。重点放在有效载荷要求和航天器总线功能的工程设计上, 在严格的系统工程框架内进行设计活动。还讨论了进一步的工作 总体任务设计,以支持DELTA-Sat的开发和运营。 DELTA-Sat演习的技术成果是对卫星进行初步设计(阶段0 /阶段A)。 由于子系统之间的权衡,微卫星和辅助任务体系结构也应运而生。子系统设计是 为有效载荷,推进,姿态确定和控制系统(ADCS),结构,热, 通信,电力系统(EPS)以及命令和数据处理系统(CDHS)方面的内容 飞船。此外,质量和动力预算,发射段和生命周期成本估算也都在其中。 定义。最终的系统创新地使用了无阻力技术,可以在较低位置进行测量 热球,同时享受微卫星提供的降低成本和缩短开发时间的优势。在 结论是,DELTA-Sat项目使学生获得了系统工程方面的宝贵经验 设计新颖的微卫星任务的方法论。最终产生的DELTA-Sat设计得益于增加的 由于子系统的协作性,导致对子系统相互依赖性和客户需求的敏感性 设计过程。

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