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Numerical modeling of the hybrid plume plasma rocketThis paper reports on ongoing research in the area of numerical simulations of hybrid plume dynamics, and describes the basic mechanisms for energy and particle transport. The solution approach assumes cylindrical geometry and includes a multiplicity of atomic reactions, as well as the presence of a strong magnetic field. The principal reactions are electron impact ionization, and resonant charge exchange between hot ions and cold neutrals. Radial particle and energy transport is mainly by diffusion. The present description includes a modified Bohm diffusion model for plasma in the core of the plume, and classical neutral particle diffusion in the cooler regions of the flow. Neutrals are allowed to 'free stream' in the low density regions, where the collision mean-free-path becomes comparable, or even larger than the characteristic dimensions of the system. A parameteric scan of the various regimes of interest has been completed and the most significant results are presented.
Document ID
19860026262
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chang, F. R.
(NASA Johnson Space Center Houston, TX, United States)
Krueger, W. A.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Yang, T. F.
(MIT Cambridge, MA, United States)
Date Acquired
August 12, 2013
Publication Date
September 1, 1985
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 85-2049
Accession Number
86A11000
Distribution Limits
Public
Copyright
Other

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