A Self-Consistent Open Boundary Condition for Fully Kinetic Plasma Thruster Plume Simulations

Document Details

Document Type
Pub Defense Publication
Publication Date
Mar 01, 2020
Source ID
10.1109/tps.2020.2968887

Entities

People

  • Deborah A. Levin
  • Revathi Jambunathan

Organizations

  • Air Force Office of Scientific Research
  • National Science Foundation

Tags

Technology Areas

  • Space
  • Space - Hall-Effect Thruster