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University of Illinois at Urbana-Champaign

Characterization of a multimode propellant operating in a porous glass electrospray thruster

Abstract

dc:description

Multimode space propulsion is an emerging technology that shows a promising increase in mission flexibility, adaptability, and mass savings for specific missions [1]. Finding a propellant that operates well in multiple propulsive modes is a key step in getting multimode propulsion systems flying in space. This study characterizes a novel multimode propellant named FAM-110A through operation in a porous glass electrospray thruster. Measurements acquired include current-voltage characteristic curves, plume ion potential via a retarding potential analyzer, and mass to charge ratio via a linear time of flight spectrometer. FAM-110A emitted more current at comparable emitter voltages as compared to EMIM-BF4. Currents of 422 μA and 305 μA were observed at voltages of +1760 V and -1730 V respectively. RPA measurements showed less field free fragmentation during thruster operation with FAM-110A and also a 0.9% average energy efficiency. During cation emission, it was found that the FAM-110A plume consists of primarily the EMIM cation with no observable evidence of the presence of HA+. Many species were found to exist in the negative emission plume including the two know anions: nitrate, and ethylsulfate. Performance parameters were calculated for each propellant. The calculations showed the thruster operating with FAM-110A produced 3.9 μN and 9.1 μN more thrust in cation and anion emission, respectively. The specific impulse of FAM-110A was 1412 seconds lower in positive mode and 1485 seconds lower in negative mode. The calculated propulsive efficiency for FAM-110A was 35.9% lower during positive mode and 21.2% lower during negative mode when compared to EMIM-BF4.

Degree

thesis:*
Name thesis:degree_name
M.S.
Level thesis:degree_level
Thesis
Discipline thesis:degree_discipline
Aerospace Engineering
Grantor
University of Illinois at Urbana-Champaign
Year dc:date
2023

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Adduci, Anthony
Contributors dc:contributor
  • Rovey, Joshua

Subjects

dc:subject × 3

Rights

dc:rights
Statement dc:rights
  • Copyright 2023 Anthony Adduci
Language dc:language
en, eng

Identifiers

dc:identifier.*
Handle dc:identifier
https://hdl.handle.net/2142/120091

Chain of custody

source
Harvested from
University of Illinois - Urbana-Champaign
Base URL
www.ideals.illinois.edu/oai-pmh
Last updated
2026-07-22
Source record
OAI-PMH GetRecord
citation

Adduci, Anthony. Characterization of a multimode propellant operating in a porous glass electrospray thruster. Thesis thesis, University of Illinois at Urbana-Champaign, 2023. https://hdl.handle.net/2142/120091