An in-flight plasma diagnostic package for spacecraft with electric propulsion

[1]  A. Piel,et al.  Foundations of measurement of electrons, ions and species fluxes toward surfaces in low-temperature plasmas , 2021 .

[2]  R. Schneider,et al.  Numerical modeling of high efficiency multistage plasma thrusters for space applications , 2019, Reviews of Modern Plasma Physics.

[3]  T. Trottenberg,et al.  An interferometric force probe for beam diagnostics and the study of sputtering , 2018 .

[4]  Quang Hoa Le,et al.  Overview of thermal arcjet thruster development , 2018 .

[5]  Publisher's Note , 2018, Anaesthesia.

[6]  L. Chen,et al.  IEDF distortion and resolution considerations for RFEA operation at high voltages , 2017 .

[7]  T. Trottenberg,et al.  Measurement and simulation of forces generated when a surface is sputtered , 2017 .

[8]  R. Schneider,et al.  Ion angular distribution simulation of the Highly Efficient Multistage Plasma Thruster , 2017, Journal of Plasma Physics.

[9]  Stéphane Mazouffre,et al.  Electric propulsion for satellites and spacecraft: established technologies and novel approaches , 2016 .

[10]  T. Trottenberg,et al.  Non-electrostatic diagnostics for ion beams and sputter effects , 2012 .

[11]  A. von Keudell,et al.  Calibration of a miniaturized retarding field analyzer for low-temperature plasmas: geometrical transparency and collisional effects , 2010 .

[12]  M. El-Gomati,et al.  High-resolution retarding field analyzer , 2003 .

[13]  H. Neumann,et al.  Effects of aperture displacement in broad-beam ion extraction systems , 2002 .

[14]  F. Scholze,et al.  A unique ECR broad beam source for thin film processing , 2001 .

[15]  David E. Brinza,et al.  Deep Space 1 Measurements of Ion Propulsion Contamination , 2001 .

[16]  M. Tajmar,et al.  Modeling of Spacecraft-Environment Interactions on SMART-1 , 2001 .

[17]  Shaun Thomson,et al.  Applying Contamination Modeling to Spacecraft Conventional Propulsion System Designs and Operations , 2001 .

[18]  James E. Polk,et al.  Deep Space One Investigations of Ion Propulsion Plasma Environment , 2000 .

[19]  G. Noci,et al.  ANELECTRIC PROPULSION DIAGNOSTIC PACKAGE FOR.THE CHARACTERIZATIQN OF TJBPLASMA THRUSTER/SPACECRAFT INTERACTIONS ON'STENTOR SATELLITE , 1999 .

[20]  J. Simpson,et al.  DESIGN OF RETARDING FIELD ENERGY ANALYZERS , 1961 .

[21]  I. Langmuir,et al.  THE THEORY OF COLLECTORS IN GASEOUS DISCHARGES , 1926 .

[22]  John E. Foster,et al.  Recommended Practice for Use of Faraday Probes in Electric Propulsion Testing , 2017 .

[23]  Tim Brandt,et al.  Simulation for an improvement of a down-scaledHEMP thruster , 2015 .

[24]  Hans-Peter Harmann,et al.  The ULAN Test Station and its Diagnostic Package for Thruster Characterization , 2007 .

[25]  N. Koch,et al.  Status of the THALES High Efficiency Multi Stage Plasma Thruster Development for HEMP-T 3050 and HEMP-T 30250 , 2007 .

[26]  Günter Dr. Kornfeld,et al.  Physics and Evolution of HEMP-Thrusters , 2007 .

[27]  Günter Kornfeld,et al.  FIRST TEST RESULTS OF THE HEMP THRUSTER CONCEPT , 2003 .

[28]  G. Yeom,et al.  Characterization of an Oxygen Plasma by Using a Langmuir Probe in an Inductively Coupled Plasma , 2001 .

[29]  J. Perrin,et al.  Retarding‐field analyzer for measurements of ion energy distributions and secondary electron emission coefficients in low‐pressure radio frequency discharges , 1993 .

[30]  S. Kitamura,et al.  Ion Thruster Charge-Exchange Plasma Flow , 1982 .