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Massachusetts Institute of Technology

Testing new potential fuels for ion electrospray propulsion systems

Abstract

dc:description.abstract

Electrospray thrusters are a class of electric propulsion that extract and accelerate ions from the surface of an electrically conductive liquid surface. This liquid surface is that of an ionic liquid, a room temperature molten salt, applied to a porous substrate. The substrate is etched via laser to form a field enhancing structure off of which ions will be evaporated. This research expands on the field in two separate ways. First, it implements and evaluates a carbon xerogel emitter substrate as an alternative over current glass emitters. This substrate was found to fire stably and with higher stable currents than the glass alternative (1.5 - 2 times the maximum stable current). In addition, this work analyzes and evaluates two new high conductivity ionic liquid propellants, EMI-(HF)F and S111-(HF)F. Improvements or disadvantages of EMI- (HF)F over the current baseline of EMI-CF₃BF₃ were inconclusive. S111-(HF)F, however, showed a distinct improvement in specific impulse over EMI-CF₃BF₃ (3160 ± 290 s vs. 2140 ± 130 s) without a statistically significant drop in total efficiency. Future work could include the collection of time of flight data in the negative firing mode, as well as higher precision retarding potential data in both positive and negative polarities. Additional measures could also be taken to decrease the spacing between emitter tips on the carbon substrate, thereby increasing the current and thrust density of the thrusters.

Degree

thesis:*
Department dc:contributor.department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics.
Grantor dc:publisher
Massachusetts Institute of Technology
Year dc:date.issued
2018

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Getty, Daniel (Daniel E.)
Advisor dc:contributor.advisor
  • Paulo Lozano.

Subjects

dc:subject × 1

Rights

dc:rights
Statement dc:rights
  • MIT theses are protected by copyright. They may be viewed, downloaded, or printed from this source but further reproduction or distribution in any format is prohibited without written permission.
Language dc:language.iso
eng

Identifiers

dc:identifier.*
Handle dc:identifier.uri
http://hdl.handle.net/1721.1/120433
OAI identifier oai:identifier
oai:dspace.mit.edu:1721.1/120433

Chain of custody

source
Harvested from
MIT
Base URL
dspace.mit.edu/oai/request
Last updated
2026-07-22
Source record
OAI-PMH GetRecord
citation

Getty, Daniel (Daniel E.). Testing new potential fuels for ion electrospray propulsion systems. Massachusetts Institute of Technology, 2018. http://hdl.handle.net/1721.1/120433