Feasibility of a Deep-Space CubeSat Mission with a Stage-Based Electrospray Propulsion System
Independent deep-space CubeSat missions require efficient propulsion systems capable of delivering several km/s of ΔV. The ion Electrospray Propulsion System under development at MIT's Space Propulsion Laboratory is a high ΔV propulsion system that is a promising technology for propulsion of in...
| Main Authors: | , , , , |
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| Format: | Article |
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Institute of Electrical and Electronics Engineers (IEEE)
2021
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| Online Access: | https://hdl.handle.net/1721.1/129473 |