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

• Published in: CEAS space journal Vol. 9; no. 1; pp. 111 - 125
• Main Authors: Cervone, A., Zandbergen, B., Guerrieri, D. C., De Athayde Costa e Silva, M., Krusharev, I., van Zeijl, H.
• Format: Journal Article
• Language: English
• Published: Vienna Springer Vienna 01.03.2017; Springer Nature B.V
• Subjects: Aerospace industry; Aerospace safety; Aerospace Technology and Astronautics; Attitude control; Computer simulation; Cubesat; Customization; Design optimization; Engineering; Expansion cards; Flight; Formation flying; Gas pressure; Heating; Missions; Molecular chains; Original Paper; Propulsion systems; Space vehicles; Spacecraft components; Thrusters; Water; Resistojet; CubeSats; Micro-propulsion; Green propellants
• ISSN: 1868-2502; 1868-2510
• DOI: 10.1007/s12567-016-0135-3

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 water-propelled 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.