Abstract
A helicon thruster was developed to research a diagnostic technique for determining plasma parameters using emission spectroscopy and helium line ratios. Conventional plasma diagnostics consisting of conductive components which contact the plasma directly can have measurement errors in the presence of radio frequency, electric, or magnetic fields. A non-invasive diagnostic technique is sought to eliminate these problems. A collisional radiative model is needed to determine the electron density and temperature that result in the measured emission line ratios. This research describes a quasi-steady state collisional radiative model used to determine the electron temperature and density in a helium helicon thruster.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
