HIGH SPECIFIC IMPULSE THERMAL ARC JET THRUSTOR TECHNOLOGY

Abstract

The MPD arcjet program at EOS is aimed at developing the technology of electric thrustors capable of performing efficiently (40-60% conversion of electrical power to beam power) for extended periods of time (up to 100 hours) in the specific impulse range of 1500-5000 seconds, at power levels of 10-100 kilowatts. The analytical results are presented for each of the significant mechanisms. Progress in the experimental portion of the program has included the following: The thrustor has been operated continuously for 100 hours with no significant electrode erosion; A novel gas-actuated feed system which had been designed during the previous reporting period was fabricated, tested and calibrated; Test runs were made using ammonia as propellant; Tests with a three- magnet configuration resulted in performance inferior to that obtained with the two-magnet thrustor.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1967
Accession Number
AD0806949

Entities

People

  • C. B. Shepard
  • G. L. Cann
  • R. L. Harder
  • S. T. Nelson

Organizations

  • Xerox

Tags

DTIC Thesaurus Topics

  • Air Force
  • Alkali Metals
  • Charged Particles
  • Electrons
  • Energy
  • Fabrication
  • Flow Rate
  • Geometry
  • High Temperature
  • Ionization Potentials
  • Life Tests
  • Magnetic Fields
  • Materials
  • Measurement
  • Specific Impulse
  • Thermal Efficiency
  • Vacuum Chambers

Fields of Study

  • Physics

Readers

  • Aerospace Propulsion Engineering.
  • Aerospace Test and Evaluation
  • Computational Modeling and Simulation