Open electric propulsion with an application to thermionic orificed hollow cathodes

Pierre Yves C.R. Taunay, Christopher J. Wordingham, Edgar Y. Choueiri

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

The concept of open data and software for electric propulsion is discussed and exemplified by an open database that contains over 40 years of thermionic orificed hollow cathode experimental data. Because scaling laws for electric propulsion devices must be verified over a wide range of operating conditions, access to data is critical. Examples of statistical analysis that can be performed with the dataset and resulting physical insights are presented. The empirical analysis conducted suggests that the ratio of total to magnetic pressure inside hollow cathodes depends on at most two other non-dimensional parameters and that the value of 3.7 Torr-cm for the total pressure-insert diameter product is likely a sufficient condition for nominal cathode operation. Solutions to increase the sharing of data and software in the electric propulsion community are suggested.

Original languageEnglish (US)
Title of host publicationAIAA Propulsion and Energy 2020 Forum
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
Pages1-10
Number of pages10
ISBN (Print)9781624106026
DOIs
StatePublished - 2020
EventAIAA Propulsion and Energy 2020 Forum - Virtual, Online
Duration: Aug 24 2020Aug 28 2020

Publication series

NameAIAA Propulsion and Energy 2020 Forum

Conference

ConferenceAIAA Propulsion and Energy 2020 Forum
CityVirtual, Online
Period8/24/208/28/20

All Science Journal Classification (ASJC) codes

  • Energy(all)
  • Aerospace Engineering
  • Control and Systems Engineering
  • Electrical and Electronic Engineering
  • Mechanical Engineering

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  • Cite this

    Taunay, P. Y. C. R., Wordingham, C. J., & Choueiri, E. Y. (2020). Open electric propulsion with an application to thermionic orificed hollow cathodes. In AIAA Propulsion and Energy 2020 Forum (pp. 1-10). (AIAA Propulsion and Energy 2020 Forum). American Institute of Aeronautics and Astronautics Inc, AIAA. https://doi.org/10.2514/6.2020-3638