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University of Illinois at Urbana-Champaign

Electrospray power processing unit for a monopropellant-electrospray multimode thruster

Abstract

dc:description

Multimode space propulsion combines two or more propulsive methods into a single system with a shared propellant, the goal of which is to offer spacecraft improved maneuver flexibility and efficiency. A power processing unit (PPU) is described and developed here to meet the high-voltage low-power needs of the electrospray mode of a monopropellant-electrospray multimode thruster. The PPU is resilient to the variable-load nature of electrospray thrusters, producing a consistent output voltage regardless of the thruster’s current draw. The PPU consists of a two-phase interleaved boost converter, transformer, and Cockcroft-Walton voltage multiplier. By designing a transformer magnetizing inductance of at least 1 mH and using a 10 MΩ bleed resistor at the PPU output, discontinuous conduction mode is avoided during the thruster startup period before Taylor cone formation. This allows the desired thruster voltage of 3.25 kV to be maintained both during and after thruster startup. A 20 MΩ current-limiting resistor placed just before the thruster prevents PPU component damage during thruster shorts. The presence of this resistor also maintains the voltage multiplier output voltage even if the thruster voltage itself cannot be sustained without overcurrent, allowing nominal electrospraying to resume if the thruster recovers from the short. The PPU is integrated with a real multimode thruster for a ground-based test to prove its suitability for the application, marking the first time a purpose-built electrospray PPU has been successfully applied to a monopropellant-electrospray multimode thruster.

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
2022

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Eisen, Jacob
Contributors dc:contributor
  • Rovey, Joshua L

Subjects

dc:subject × 7

Rights

dc:rights
Statement dc:rights
  • Copyright 2022 Jacob Eisen
Language dc:language
en, eng

Identifiers

dc:identifier.*
Handle dc:identifier
https://hdl.handle.net/2142/117846

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

Eisen, Jacob. Electrospray power processing unit for a monopropellant-electrospray multimode thruster. Thesis thesis, University of Illinois at Urbana-Champaign, 2022. https://hdl.handle.net/2142/117846