Demonstration Tests And An Analysis Of Critical Issues Associated With Low Power TAL

Abstract

This report results from a contract tasking TSNIIMASH - EXPORT, JSC as follows: The goal of proposed SOW is to demonstrate current status and performances of low power (0.1...1 kW) Thrusters with Anode Layer ( TAL) with using Xenon propellant, provide an analysis of critical issues associated with low power TAL development and potential level of low power TAL characteristics, propose draft of the program for breadboard low power thruster development.

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Document Details

Document Type
Technical Report
Publication Date
Jan 25, 2000
Accession Number
ADA464614

Entities

People

  • Alexander V. Semenkin

Tags

Communities of Interest

  • Advanced Electronics
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Artificial Satellites
  • Demonstrations
  • Dielectrics
  • Electric Fields
  • Electric Propulsion
  • Energy Consumption
  • Flow Rate
  • Geometry
  • Guard Rings
  • Hall Thrusters
  • Magnetic Fields
  • Power Supplies
  • Propulsion Systems
  • Small Satellites
  • Spacecraft
  • Test Facilities
  • Voltage

Readers

  • Aerospace Propulsion Engineering.
  • Software Engineering

Technology Areas

  • Space
  • Space - Hall-Effect Thruster