Exploring Energy Conversion and Transport in RF-Driven of Molecular Gas Plasmas through Modeling and Simulation

Abstract

As the commercialization of electric propulsion (EP) thrusters has expanded, xenon and other noble gases have become resource limited quantities. As a substitute, a number of molecular propellants are under consideration for future envisioned EP systems, particularly those produced using higher number density RF driven sources. However, there are important fundamental science gaps in the plasmadynamics of such thruster systems that need to be addressed. The proposed research encompasses three general elements that will allow us to understand the physics of RF- fed magnetically focused molecular plasmas. (1) The energy conversion and transport of a simple RF-fed source into an Inductively Coupled Plasmas (ICPs), joined by a subsonic-supersonic nozzle will be studied. This will enable us to understand how the boundary layer and any frozen flow losses affect plasma expansions. Type 1 molecular propellants will be studied in the proposed work since there a number of internal energy mode transfer models that already exist for air-derived molecules. (2) Energy conversion for the same atomic and molecular gases will then be considered for an ECR microwave plasma source. We will investigate how zones of strong magnetic fields excite the molecular plasma and considering the higher plasma number density compared to the ICP-nozzle case, how does the thermalization of electrons change internal energy losses. The more complex nature of the RF coupling into the plasma and its effect on heating electrons will be considered. (3) To obtain information about the role of internal energy transfer in molecular plasmas, a general collisional radiative (CR) model to predict optical emission spectra will be developed. The CR model will build on previously processes known to be important in argon and xenon as well as earth reentry plasmas.

Document Details

Document Type
DoD Grant Award
Publication Date
Feb 06, 2025
Source ID
FA95502510052

Entities

People

  • Deborah Ann Levin

Organizations

  • Air Force Office of Scientific Research
  • United States Air Force
  • University of Illinois Urbana–Champaign

Tags

Fields of Study

  • Physics

Readers

  • Aerospace Propulsion Engineering.
  • Plasma Physics.
  • Systems Analysis and Design

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight
  • Microelectronics
  • Space
  • Space - Hall-Effect Thruster