Plasma-Gas Interaction Studies in a Hybrid Plume Plasma Rocket.

Abstract

This report discusses the progress in the fluid modeling of a hybrid plume plasma rocket and the heating of plasma in a tandem mirror device. In the theoretical area three tasks have been accomplished: 1) A major advance has been made in the development of a numerical method for solving the time dependent fluid equations for both ions and electrons in the plasma. 2) A mathematical model has been formulated for studying the radio frequency heating of the hot plasma in cylindrical geometry. 3) An analysis on the performance characteristics of the hybrid plume rocket has been carried out. Under the funding of the instrumentation program the component fabrication is on progress. The coils have been delivered. Keywords: Plasma propulsion.

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Document Details

Document Type
Technical Report
Publication Date
Sep 30, 1987
Accession Number
ADA190310

Entities

People

  • F. R. Chang-diaz
  • T. F. Yang

Organizations

  • Massachusetts Institute of Technology

Tags

Communities of Interest

  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Assembly
  • Cyclotron Resonance
  • Efficiency
  • Electromagnetic Fields
  • Electrons
  • Equations
  • Fabrication
  • Frequency
  • Geometry
  • Instrumentation
  • Magnetic Fields
  • Payload
  • Plasma Engines
  • Power Levels
  • Radio Frequency Power
  • Two Dimensional
  • Vacuum Chambers

Fields of Study

  • Physics

Readers

  • Computational Fluid Dynamics (CFD)
  • Plasma Physics / Magnetohydrodynamics
  • Rocket Propulsion.

Technology Areas

  • Microelectronics