This final report summarizes the research carried out on the development of numerical approaches for simulating the plumes of electric propulsion devices. In Appendix I, we describe the development of a particle based Monte Carlo approach for simulating the plumes and impingement of chemical propulsion systems, in Appendix II, we describe a plume model for an electric propulsion device (a Hall thruster). The research performed in this grant has led to significant advances in the capabilities for modeling these plume flows.
Modeling of an Arcjet Plume for Thin Film Synthesis
2000
23 pages
Report
No indication
English
Fluctuation of Arcjet Plume Properties
Online Contents | 1996
|Fluctuation of arcjet plume properties
AIAA | 1996
|Plume characteristics of an arcjet thruster
NTRS | 1993
|Plume characteristics of an arcjet thruster
AIAA | 1993
|Ceramic thin film synthesis via arcjet CVD
AIAA | 1995
|