Fundamental experiments on electrospray propulsion: Propellants, plumes, and material interactions

Lyne, Christopher

Permalink

https://hdl.handle.net/2142/124615 Copy

Description

Title

Fundamental experiments on electrospray propulsion: Propellants, plumes, and material interactions

Author(s)

Lyne, Christopher

Issue Date

2024-01-08

Director of Research (if dissertation) or Advisor (if thesis)

Rovey, Joshua

Doctoral Committee Chair(s)

Rovey, Joshua

Committee Member(s)

• Levin, Deborah
• Elliott, Gregory
• Liu, Thomas

Department of Study

Aerospace Engineering

Discipline

Aerospace Engineering

Degree Granting Institution

University of Illinois at Urbana-Champaign

Degree Name

Ph.D.

Degree Level

Dissertation

Keyword(s)

• Electrospray Propulsion
• Ion Beam Diagnostics
• Mass Spectrometry

Language

eng

Abstract

Electrospray sources are devices that use electric fields to extract charged particles directly from a liquid surface. Those charged particles may span a large mass range, from single molecular ions (10^2 amu/q) to large droplets (>10^5 amu/q), depending on the type of electrospray source and its operating conditions. Species in electrospray plumes are heavier than most ion sources (e.g., a Hall-effect thruster), making electrospray appealing for applications such as spacecraft propulsion and material etching. The distribution of mass and energy within the plume determines the performance of an ion source for a given application. In a propulsion context, those distributions may be used to calculate thrust, specific impulse, and efficiency. However, accurately measuring those distributions can be challenging. Part 1 of this dissertation describes a tandem energy analyzer/mass spectrometer for measuring the mass and energy distributions in electrospray plumes. The instrument was used to characterize a capillary emitter plume and the plume of an ionic liquid ion source (ILIS). The ILIS data was used to calculate the mean lifetime of ion clusters in the electrospray plume. For the ILIS used here, operated with the ionic liquid EMI-BF4, we calculate that the EMI+[EMI][BF4] dimer mean lifetime ranges from 3.5 ns to 142 ns for electric field strengths ranging from 35 V/µm to 2 V/µm, respectively. Similarly, the EMI+([EMI][BF4])2 trimer has an estimated lifetime of 0.9 ns to 13 ns for electric field strengths ranging from 22 V/µm to 2 V/µm, respectively. From those data, we estimate the temperature and solvation energy of positive EMI-BF4 dimers is T=471±216 K and ΔG=0.62±0.26 eV, respectively. Similarly, for positive trimers we estimate that T=475±422 K and ΔG=0.55±0.43 eV. These results are among the first to use empirical methods to estimate EMI-BF4 cluster lifetimes, temperature, and solvation energy. Part 2 of this dissertation discusses other topics in electrospray propulsion. We present a “Secondary Species Emission" (SSE) probe designed to measure secondary charge emission from surfaces bombarded by electrospray plumes. Further, we demonstrate that the SSE probe can be operated in tandem with the energy analyzer/mass spectrometer to measure SSE yield as a function of the mass and energy of incident plume species. The ability to discriminate between different species and energies is a novel and significant advance in secondary charge emission measurements. Part 2 continues, presenting the first successful demonstration of a prototype thruster that combines electrospray and monopropellant functionality into a single device. Finally, Part 2 concludes with an investigation of water removal from ionic liquid electrospray propellants.

Graduation Semester

2024-05

Type of Resource

Text

Handle URL

https://hdl.handle.net/2142/124615

Copyright and License Information

Copyright 2023 Christopher Lyne

Owning Collections