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Liquid-metal-ion source development for space propulsion at ARC.

M Tajmar1, C Scharlemann, A Genovese

  • 1Space Propulsion & Advanced Concepts, Austrian Research Centers GmbH-ARC, Austria. martin.tajmar@arcs.ac.at

Ultramicroscopy
|December 10, 2008
PubMed
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Austrian Research Centers developed indium Liquid-Metal-Ion Sources (LMIS) for space propulsion, achieving over 4800 hours of operation. New porous multi-tip designs aim for significantly higher currents for enhanced space thruster performance.

Area of Science:

  • Spacecraft engineering
  • Materials science
  • Plasma physics

Background:

  • The Austrian Research Centers have extensive experience in developing indium Liquid-Metal-Ion Sources (LMIS).
  • LMIS technology is crucial for various space applications, including spacecraft charging compensators, Secondary Ion Mass Spectrometry (SIMS), and propulsion systems.
  • High-current and long-term operational stability are critical challenges for LMIS in space propulsion.

Purpose of the Study:

  • To address the challenges of long-term, high-current operation of LMIS for space propulsion.
  • To present advancements in LMIS technology, including single-tip and multi-tip designs.
  • To analyze and model key performance factors like tip erosion and droplet deposition.

Main Methods:

  • Demonstration of a cluster of single LMIS operating at an average current of 100 μA for over 4800 hours.

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  • Development of predictive models for tip erosion and droplet deposition.
  • Design and development of a porous multi-tip LMIS for significantly increased current output (up to several mA).
  • Main Results:

    • Successful long-term operation of single LMIS exceeding 4800 hours at 100 μA.
    • Models suggest potential operational lifetimes of 20,000 hours or more for single LMIS.
    • Development of a porous multi-tip source capable of achieving significantly higher currents.

    Conclusions:

    • Indium LMIS technology is viable for demanding space propulsion applications.
    • Further development of multi-tip LMIS is promising for achieving the high-current requirements of space thrusters.
    • Understanding and mitigating tip erosion and droplet deposition are key to maximizing LMIS lifespan and performance.