Plasma diagnostic with inductive probes in the discharge channel of a pulsed plasma thruster-Reference-Cited by-同舟云学术

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Plasma diagnostic with inductive probes in the discharge channel of a pulsed plasma thruster

Published:2014-12 Issue: Volume:110 Page:165-171
ISSN:0042-207X
Container-title:Vacuum
language:en
Short-container-title:Vacuum

Author:

Lau Matthias,Herdrich Georg

Funder

Bundesministerium für Wirtschaft und Technologie

Deutsches Zentrum für Luft- und Raumfahrt

Publisher

Elsevier BV

Subject

Surfaces, Coatings and Films,Condensed Matter Physics,Instrumentation

Reference18 articles.

1. Ablative PPT. New quality, new perspectives;Popov;Acta Astronaut,2006

2. Thrust efficiency optimization of SIMP-LEX;Nawaz,2008

3. Scaling laws for pulsed electric propulsion with application to the pluto express mission;Ziemer,1995

4. Multi-axis thrust measurement of the EO-1 pulsed plasma thrusters;Arrington,1999

5. Physics of electric propulsion;Jahn,1968

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1. Analysis of composition and dynamics of the plasma plume emitted by a 1 J pulsed plasma thruster fed with polytetrafluoroethylene and determination of thruster efficiency components;Physics of Plasmas;2024-05-01

2. Study on the influence of ignitor position on a coaxial pulsed plasma thruster;Vacuum;2023-12

3. Transient buildup and dissipation of a compressed plasma shockwave in arc-discharge plasma beams;Plasma Sources Science and Technology;2021-12-01

4. The ablation characteristics of laser-assisted pulsed plasma thruster with metal propellant;Plasma Science and Technology;2021-09-02

5. Study on propellant utilization in pulsed plasma thrusters;Acta Astronautica;2021-05

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