[HTML][HTML] Positive and negative secondary species emission behavior for an ionic liquid electrospray

NM Uchizono, C Marrese-Reading, SM Arestie… - Applied Physics …, 2022 - pubs.aip.org
Ionic liquid electrosprays can emit a polydisperse population of charged droplets, clusters,
and molecular ions at high velocity. Secondary species emission (SSE) is a term that …

Characterization of a Single Emitter Passively Fed Electrospray Ion Source: Part II-Luminescence Spectral Analysis

TV Kerber, NJ Allwine, K Lemmer… - Journal of Physics D …, 2025 - iopscience.iop.org
Luminescence spectroscopy was used to examine the dynamics of propellant dissociation
near the emitter tip of a single-emitter porous electrospray thruster loaded with the ionic …

[PDF][PDF] Plume study of an electrospray thruster using a HAN-based dual-mode ionic liquid propellant

C Ma, V Messina, CN Ryan, JL Rovey… - Proceedings of the …, 2022 - eplab.ae.illinois.edu
This paper investigates the electrospray performance of FAM-110A, a novel
hydroxylammonium nitrate (HAN) based ionic liquid propellant developed for a chemical …

Optical emission characterization of a single emitter electrospray thruster interacting with surfaces

N Turan, C Ma, CN Ryan - AIAA SCITECH 2023 Forum, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-1409. vid Electrospray thrusters
are a promising small satellite electric propulsion system, capable of emitting ions with …

[PDF][PDF] Development of Porous Emitter Electrospray Thruster Using Advanced Manufacturing Processes

A Quraishi, S Dworski, C Ma, C Ryan, A Ferreri… - 2022 - researchgate.net
In the past decade, nanosatellites (eg, satellites with a mass of 1–20 kg) have become
increasingly popular and now account for a significant portion of global satellite launches [1] …