Long-Life C12A7 Heaterless Cathode for Electric Propulsion Thrusters

Abstract

Since 2017, a heaterless hollow cathode has been developed at the Technische Universitaet Dresden, using the emitter C12A7 electride [Ca24Al28O64]4 (4e-). During this time, many findings have been reported in the corresponding interim reports. The primary accomplishment of this research was the development and research towards achieving C12A7 cathode Hull thruster neutralizer operating at 2 Amps for 950 hours before running out of propellant gas (i.e. the neutralizer cathode did not stop working -- just experiment ran out of gas and stopped experiment). This report will give a detailed overview of the development of the hollow cathode and the achievements and results in the corresponding work packages over the course of the entire project. Some findings during the last year with the zero cost extension will be added as well as dedicated discussions to the work packages itself.

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Document Details

Document Type
Technical Report
Publication Date
Mar 02, 2022
Accession Number
AD1165541

Entities

People

  • C. Drobny
  • J. P. Wulfkuehler
  • Martin Tajmar
  • N. Gondol

Tags

Communities of Interest

  • Advanced Electronics
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Aging (Materials)
  • Air Force Research Laboratories
  • Climate Change
  • Coefficients
  • Composite Materials
  • Electric Propulsion
  • Electrical Conductivity
  • Electron Emission
  • Electrons
  • Emitters
  • Hall Effect
  • Hall Thrusters
  • Long Life
  • Manufacturing
  • Material Degradation Processes
  • Materials
  • Materials Processing
  • Measurement
  • Space Propulsion
  • Temperature Gradients
  • Test And Evaluation
  • Thermal Conductivity
  • Thermionic Emission
  • Thrusters

Readers

  • Aerospace Propulsion Engineering.
  • Electronics Engineering
  • Technical Research and Report Writing.

Technology Areas

  • Space
  • Space - Hall-Effect Thruster