TY - GEN
T1 - Characterization of inductively coupled RF plasma source operating with molecular gases for electric propulsion
AU - Ussenov, Y. A.
AU - Raitses, Y.
N1 - Publisher Copyright:
© 2025, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2026
Y1 - 2026
N2 - Inductively coupled radio-frequency (RF-ICP) plasma sources are widely used in semiconductor processing, mass spectrometry, nanomaterial synthesis, and also in space propulsion, where they operate across pressures from mTorr to atmospheric and power levels from tens of watts to tens of kilowatts. RF-ICPs offer an electrode-free, magnetic-field-free design that is simpler and lighter than helicon or electron-cyclotron-resonance sources, while advanced configurations with ferrite cores can achieve competitive ionization efficiency. This work develops and characterizes a low-pressure (≤10 mTorr), low-power (up to 250 W) RF-ICP source to maximize ionization of molecular gases with potential application to space propulsion such as plasma thrusters and cathodes with molecular propellant.
AB - Inductively coupled radio-frequency (RF-ICP) plasma sources are widely used in semiconductor processing, mass spectrometry, nanomaterial synthesis, and also in space propulsion, where they operate across pressures from mTorr to atmospheric and power levels from tens of watts to tens of kilowatts. RF-ICPs offer an electrode-free, magnetic-field-free design that is simpler and lighter than helicon or electron-cyclotron-resonance sources, while advanced configurations with ferrite cores can achieve competitive ionization efficiency. This work develops and characterizes a low-pressure (≤10 mTorr), low-power (up to 250 W) RF-ICP source to maximize ionization of molecular gases with potential application to space propulsion such as plasma thrusters and cathodes with molecular propellant.
UR - https://www.scopus.com/pages/publications/105031184735
UR - https://www.scopus.com/pages/publications/105031184735#tab=citedBy
U2 - 10.2514/6.2026-2815
DO - 10.2514/6.2026-2815
M3 - Conference contribution
AN - SCOPUS:105031184735
SN - 9781624107658
T3 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2026
BT - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2026
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2026
Y2 - 12 January 2026 through 16 January 2026
ER -