首页> 外文会议>International Astronautical Congress >DELTA-SAT: THE CONCURRENT PRE-PHASE A DESIGN OF A THERMOSPHERIC EXPLORATION MICROSATELLITE
【24h】

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

机译:Delta-SAT:热散勘探微卫星的并发预阶段设计

获取原文

摘要

The ‘Microsatellite Engineering' Master course at the Faculty of Aerospace Engineering of the Delft University of Technology aims to bridge the gap between education and professional engineering practise by using a projectbased approach to space systems engineering education. The course comprised of a mission and microsatellite design project, using collaborative engineering methodologies to achieve the design of a thermospheric exploration microsatellite. 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 a microsatellite. 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 addressed overall 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 a microsatellite and supporting mission architecture as a result of subsystem trade-offs. Subsystem designs were defined 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 the spacecraft. Additionally, mass and power budgets, a launch segment, and a life cycle cost estimation were also defined. The resulting system makes innovative use of drag-free technology to undertake measurements in the lower thermosphere, while enjoying the advantages of reduced cost and development time offered by microsatellites. In conclusion, the DELTA-Sat project allowed students to gain valuable experience in systems engineering methodologies by designing a novel microsatellite mission. The resulting DELTA-Sat design benefits from increased sensitivity to subsystem interdependency and customer requirements, resulting from the collaborative nature of the design process.
机译:代尔夫特理工大学航空航天工程科学工程学院的“微卫星工程”课程旨在利用投影系统工程教育的预定方法弥合教育与专业工程实践的差距。该课程包括一个使命和微卫星设计项目,采用协同工程方法来实现热散勘探微卫星的设计。本文详细说明了设计过程,由此产生了这个微卫星的技术设计,'delta-sat'。该项目工作旨在同时对微卫星的物理和功能架构的概念设计。重点是乘坐航天器总线功能的有效载荷要求和工程,在严格的系统工程框架内发生设计活动。进一步的工作还解决了整体任务设计,以支持Delta-Sat的发展和运营。 Delta-SAT练习的技术结果是微卫星的初步阶段(第0阶段/预先阶段A)设计,并且由于子系统权衡而支持任务架构。子系统设计被定义为有效载荷,推进,姿态确定和控制系统(ADC),结构,热,通信,电力系统(EPS)以及航天器的数据处理系统(CDHS)方面。此外,还定义了质量和电力预算,发射段和生命周期成本估计。由此产生的系统使无阻力技术进行了创新使用,在较低的热层中进行测量,同时享受微卫星提供的成本和开发时间的优点。总之,三角洲-SAT项目允许学生通过设计新颖的微卫兵使命,获得系统工程方法中的宝贵经验。由此产生的Delta-SAT设计与子系统相互依赖性和客户要求的敏感度增加,由设计过程的协作性质产生。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号