Advanced Electric Propulsion MPD (Magnetoplasmadynamic)

Abstract

Mangnetoplasmadynamic (MPD) thrusters are inherently low thrust devices, consequently operation for hundreds to thousands of hours will be required to impart useful levels of total impulse. Experience at Princeton and in other laboratories indicates that the cathode of these devices suffers the most severe damage in the hostile environment of the high current discharge, therefore representing the life-limiting component. To explore the physical mechanisms responsible for cathode degradation, a new diagnostic tool has been developed - the surface layer activation (SLA) technique - to monitor erosive loss. This method was chosen in the Phase I portion of this contract from several alternatives because it provides highly accurate, in-situ measurements of erosive mass loss and can be readily applied to a wide variety of materials and environments. Concurrent programs of erosion measurement on experimental MPD thrusters using this technique and supporting analytical modelling of the erosion process are now being pursued.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
May 01, 1988
Accession Number
ADA199825

Entities

People

  • A. J. Kelly
  • J. Polk
  • R. G. Jahn

Organizations

  • Princeton University

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Force
  • Contracts
  • Degradation
  • Electric Propulsion
  • Energy
  • Engineering
  • Environment
  • Gamma Ray Spectra
  • Gamma Rays
  • Magnetoplasmadynamic Thrusters
  • Materials
  • Measurement
  • Nuclear Reactions
  • Radiation
  • Spectrum Analysis
  • Steady State
  • Thrusters

Fields of Study

  • Physics

Readers

  • Aerospace Propulsion Engineering.
  • Reinforced Composite Materials
  • Systems Analysis and Design

Technology Areas

  • Space
  • Space - Hall-Effect Thruster