M. Fehringer

Observation of nuclear fusion driven by a pyroelectric crystal

Micropropulsion for small spacecraft: a new challenge for field effect electric propulsion and microstructured liquid metal ion sources

Evolution from Threshold of a Hollow Atom's X-Ray Emission Spectrum: The CuKhα1,2Hypersatellites

Complex (dusty) plasmas: Current status, open issues, perspectives

Cathode spots of electric arcs

Gravity field contribution analysis of GOCE gravitational gradient components

Parabolic Plasma Sheath Potentials and their Implications for the Charge on Levitated Dust Particles

Collinear Three-Craft Coulomb Formation Stability Analysis and Control

Analytical Charge Analysis for Two- and Three-Craft Coulomb Formations

Linear Dynamics and Stability Analysis of a Two-Craft Coulomb Tether Formation

GOCE gravitational gradiometry

Electrical discharges in vacuum: 1980-90

Collisions of atoms and ions with surfaces under grazing incidence

Production of hollow atoms by the excitation of highly charged ions in interaction with a metallic surface

Vacuum arc ion sources

Terminal Guidance System for Satellite Rendezvous

Reply to “A comment on “A test of general relativity using the LARES and LAGEOS satellites and a GRACE Earth gravity model, by I. Ciufolini et al.””

State-selective electron capture in collisions of He²⁺with H

Optical excitations in electron microscopy

Direct measurement and analysis of the carrier-envelope phase in light pulses approaching the single-cycle regime

Helium, iron, and electron particle transport and energy transport studies on the Tokamak Fusion Test Reactor

Inelastic H⁺-Li(2s) collisions (2-20 keV). II. Electron capture into H(2p) and H(3,l) subshells

A LIQUID METAL ION SOURCE FOR SPACE APPLICATION

Active spacecraft potential control for Cluster – implementation and first results

The Cluster mission

An experiment to study and control the Langmuir sheath around INTERBALL-2

Results from active spacecraft potential control on the Geotail spacecraft

Auger Electron Emission from Slow Multicharged Ions Near a Metal Surface

Spacecraft potential control aboard Equator-S as a test for Cluster-II

Electron emission from a metal surface bombarded by slow highly charged ions

<i>Introduction</i>The Cluster mission

Mission design, operation and exploitation of the gravity field and steady-state ocean circulation explorer mission