Feasibility of a Deep-Space CubeSat Mission with a Stage-Based Electrospray Propulsion System The MIT Faculty has made this article openly available. Please share how this access benefits you. Your story matters. Citation Jia-Richards, Oliver et al. "Feasibility of a Deep-Space CubeSat Mission with a Stage-Based Electrospray Propulsion System." 2020 IEEE Aerospace Conference, March 2020, Big Sky, Montana, Institute of Electrical and Electronics Engineers, August 2020. © 2020 IEEE As Published http://dx.doi.org/10.1109/aero47225.2020.9172544 Publisher Institute of Electrical and Electronics Engineers (IEEE) Version Author's final manuscript Citable link https://hdl.handle.net/1721.1/129473 Terms of Use Creative Commons Attribution-Noncommercial-Share Alike Detailed Terms http://creativecommons.org/licenses/by-nc-sa/4.0/ Feasibility of a Deep-Space CubeSat Mission with a Stage-Based Electrospray Propulsion System Oliver Jia-Richards and Paulo C. Lozano David C. Sternberg, Daniel Grebow, and Swati Mohan Space Propulsion Laboratory Jet Propulsion Laboratory Massachusetts Institute of Technology California Institute of Technology Cambridge, MA, 02139 Pasadena, CA, 91109 foliverjr,
[email protected] fdavid.c.sternberg, daniel.grebow,
[email protected] Abstract—Independent deep-space exploration with CubeSats, 1. INTRODUCTION where the spacecraft independently propels itself from Earth orbit to deep-space, is currently not possible due to the lack The exploration of small asteroids through the use of minia- of high-∆V propulsion systems compatible with the small form ture spacecraft such as CubeSats could provide substantial factor. The ion Electrospray Propulsion System (iEPS) un- benefits in terms of affordability, visit rates, and overall der development at the Massachusetts Institute of Technology’s science return.