Jove
Visualize
Contact Us
JoVE
x logofacebook logolinkedin logoyoutube logo
ABOUT JoVE
OverviewLeadershipBlogJoVE Help Center
AUTHORS
Publishing ProcessEditorial BoardScope & PoliciesPeer ReviewFAQSubmit
LIBRARIANS
TestimonialsSubscriptionsAccessResourcesLibrary Advisory BoardFAQ
RESEARCH
JoVE JournalMethods CollectionsJoVE Encyclopedia of ExperimentsArchive
EDUCATION
JoVE CoreJoVE BusinessJoVE Science EducationJoVE Lab ManualFaculty Resource CenterFaculty Site
Terms & Conditions of Use
Privacy Policy
Policies

Related Experiment Videos

Kink instability in applied-field magneto-plasma-dynamic thrusters.

M Zuin1, R Cavazzana, E Martines

  • 1Consorzio RFX, Associazione EURATOM-ENEA sulla fusione, corso Stati Uniti 4, 35127 Padova, Italy.

Physical Review Letters
|July 13, 2004
PubMed
Summary
This summary is machine-generated.

Related Concept Videos

You might also read

Related Articles

Articles linked to this work by shared authors, journal, and citation graph.

Sort by
Same author

Visible cameras as a tool to study electron beam shape.

The Review of scientific instruments·2025
Same author

Development of fast 2.5 MeV neutron detectors for high-intensity stray magnetic field environments.

The Review of scientific instruments·2024
Same author

Role of radiation re-absorption in the thermal helium beam diagnostic.

The Review of scientific instruments·2024
Same author

Spatially resolved diagnostics for optimization of large ion beam sources.

The Review of scientific instruments·2022
Same author

Development and first operation of a cavity ring down spectroscopy diagnostic in the negative ion source SPIDER.

The Review of scientific instruments·2021
Same author

Visible cameras as a non-invasive diagnostic to study negative ion beam properties.

The Review of scientific instruments·2021

A magneto-plasma-dynamic thruster

Area of Science:

  • Plasma physics
  • Space propulsion engineering

Background:

  • Magneto-plasma-dynamic (MPD) thrusters are a type of electric propulsion system.
  • MPD thrusters are being considered for space missions due to their high thrust capabilities.

Purpose of the Study:

  • To investigate the instability of magnetic and electrostatic fluctuations in an applied field MPD thruster.
  • To understand the relationship between thruster performance and plasma instabilities.

Main Methods:

  • Measurements of magnetic and electrostatic fluctuations were taken in an applied field MPD thruster.
  • The Kruskal-Shafranov limit was used as a reference for instability.

Main Results:

  • An m/n=1/1 kink mode was found to become unstable when the Kruskal-Shafranov limit is violated.

Related Experiment Videos

  • A positive correlation was observed between the kink instability and performance degradation at high currents.
  • Conclusions:

    • The identified kink instability is a key factor limiting the performance of MPD thrusters.
    • This instability has historically prevented the use of MPD thrusters in space missions.