Abstract
A mixture of [Emim][EtSO4]-HAN is a potential propellant suitable in a multi-mode chemical-electric microtube-electrospray micro propulsion system. This paper reports experimental mass spectrum results for this liquid when electro sprayed in a 50 μm capillary emitter. Mass spectra from 0-600 amu were obtained over a variety of angles and flow rates from 2 pL/sec to 3 nL/sec in both cation and anion extraction mode. Effects of flow rate and angular orientation on the spectra agree well with literature. Results show at least three of the four monomer species are emitted, along with numerous other species, some of which have been identified. Results also show, for the first time, emission of both proton-transferred covalent species paired with both ionic species for HAN. Also, because the liquid is a mixture, swapping of anions and cations between constituents is observed. This swapping is most evident in anion mode, where numerous forms of HAN ([HNO3], 2[HNO3], 2[HA-H], and [HAN]) appear in the spectra attached with [EtSO4]-. Numerous peaks in the spectra remain unidentified but are speculated to be impurities and fragments.
Recommended Citation
M. J. Wainwright et al., "Electrospray Mass Spectroscopy of a Han-Based Monopropellant," 2018 Joint Propulsion Conference, article no. AIAA 2018-4725, American Institute of Aeronautics and Astronautics, Jan 2018.
The definitive version is available at https://doi.org/10.2514/6.2018-4725
Department(s)
Mechanical and Aerospace Engineering
Publication Status
Full Access
International Standard Book Number (ISBN)
978-162410570-8
Document Type
Article - Conference proceedings
Document Version
Citation
File Type
text
Language(s)
English
Rights
© 2024 American Institute of Aeronautics and Astronautics, All rights reserved.
Publication Date
01 Jan 2018
Comments
National Aeronautics and Space Administration, Grant NNM15AA09A