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Green micro-resistojet research at Delft University of Technology: new options for Cubesat propulsion

机译:Delft技术大学的绿色微型电阻研究:CubeSat推进的新选择

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摘要

The aerospace industry is recently expressing a growing interest in green, safe and non-toxic propellants for the propulsion systems of the new generation of space vehicles, which is especially true in the case of Cubesat micro-propulsion systems. Demanding requirements are associated to the future missions and challenges offered by this class of spacecraft, where the availability of a propulsion system might open new possibilities for a wide range of applications including orbital maintenance and transfer, formation flying and attitude control. To accomplish these requirements, Delft University of Technology is currently developing two different concepts of waterpropelled micro-thrusters based on MEMS technologies: a free molecular micro-resistojet operating with sublimating solid water (ice) at low plenum gas pressure of less than 600 Pa, and a more conventional micro-resistojet operating with liquid water heated and vaporized by means of a custom designed silicon heating chamber. In this status review paper, the current design and future expected developments of the two micro-propulsion concepts is presented and discussed, together with an initial analysis of the expected performance and potential operational issues. Results of numerical simulations conducted to optimize the design of the heating and expansion slots, as well as a detailed description of the manufacturing steps for the conventional micro-resistojet concept, are presented. Some intended steps for future research activities, including options for thrust intensity and direction control, are briefly introduced.
机译:航空航天工业最近对新一代空间车辆的推进系统表达了对绿色,安全和无毒推进剂的兴趣,这在立方体微型推进系统的情况下尤其如此。苛刻的要求与这类航天器提供的未来任务和挑战有关,其中推进系统的可用性可能为各种应用开辟新的可能性,包括轨道维护和转移,形成飞行和态度控制。为实现这些要求,代尔夫特理工大学目前正在基于MEMS技术开发两种不同的潜水微推进概念:在低增长固体水(冰)下,在低于600Pa的低内升固体水(ICE)的自由分子微蚀器,并且通过定制设计的硅加热室加热和蒸发的具有更传统的微电阻器,通过定制设计的硅加热室。在此状态审查纸上,提出和讨论了两种微型推进概念的当前设计和未来预期发展,并讨论了对预期绩效和潜在运营问题的初步分析。提出了对优化加热和膨胀槽设计的数值模拟的结果,以及传统微电阻概念的制造步骤的详细描述。简要介绍了未来研究活动的一些预期步骤,包括推力强度和方向控制的选项。

著录项

  • 来源
    《CEAS Space Journal》 |2017年第1期|共15页
  • 作者单位

    Space Systems Engineering Aerospace Engineering Faculty Delft University of Technology Kluyverweg 1 2629 HS Delft The Netherlands;

    Space Systems Engineering Aerospace Engineering Faculty Delft University of Technology Kluyverweg 1 2629 HS Delft The Netherlands;

    Space Systems Engineering Aerospace Engineering Faculty Delft University of Technology Kluyverweg 1 2629 HS Delft The Netherlands;

    Space Systems Engineering Aerospace Engineering Faculty Delft University of Technology Kluyverweg 1 2629 HS Delft The Netherlands;

    Space Systems Engineering Aerospace Engineering Faculty Delft University of Technology Kluyverweg 1 2629 HS Delft The Netherlands;

    Else Kooi Laboratory Electrical Engineering Mathematics and Computer Science Faculty Delft University of Technology Feldmanweg 17 2628 CT Delft The Netherlands;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航天(宇宙航行);
  • 关键词

    Micro-propulsion; Resistojet; CubeSats; Green propellants;

    机译:微型推进;抵抗力;立方体;绿色推进剂;

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