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elektrischer Antrieb
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Modelling of Battery-PWM-Invertor-PM Synchronous Motor for Vehicle Drive chain
Interaction between Plasma Plume of Electric Propulsion and Spacecraft Communication
Application of DC Arcjet for Low Earth Orbit Spacecraft
Own Magnetic Field Impact on MPD Thrusters Performance with External Magnetic Field
Scaling Law Applicable to Design of MPD Arcjet
Low Power, Hall Thruster Propulsion System
An Approach to Arcjet Thruster Computations for Faster Convergence
Titanium Optics for Ion Thrusters
Plume Study of Multimode Thruster SPT-140
Researches for Reaching Minimum Thrusts in Regulates Monofuel Micro Liquid Propulsion Thrusters
Plasma Diagnostics of Laser Sustained Plasma in a CW Laser Thruster
Numerical Study of Onset Phenomena in a 2-Dimensional Axisymmetric MPD Thruster
Development and Performance Testing of an RF-Ion Thruster for Primary Propulsion
Development of A "Smart" Power Processing Unit for Hall Effect Thrusters
Contamination Sensor for Electric Propulsion and Solid Rocket Motor
System Considerations of Electrodynamic-Tether Propulsion Technology and Future Plans
Evaluation of Electrodynamic Tether Propulsion to OTV
Pulsed Plasma Thrusters for Spacecraft Attitude and Orbit Control System
Temperature and Material Effects on the Operation of MPD Cathodes
Computation of Hall Thruster Performance
CFD Analysis of Plasma Flow in a Laser Thruster
Use of Composite Propellants as for Electric Thrusters
Experimental Analysis of a Solid Propellant MPD Thruster with Different Anode Radii
Cathode Jet of Magnetoplasmadynamic Thrusters
Electrode Power Loss and Thruster Performance of a Pulsed MPD Accelerator
A Xenon Propellant Management sub-Unit for Ion Propulsion
Development of an Ion Thruster Control Unit for the MUSES-C Mission
Improvement of 20mN Xenon Ion Thruster
Development of an RF-Ion Thruster for Commercial Application
Development of a MHD Code Using CIP Method and Its Application to a Laser Fusion Rocket
The USAF Electric Propulsion Program
An Overview of the On-Orbit Results from the Electric Propulsion Space Experiment
Numerical Analyses of MHD Flows in an Applied-Field MPD Arcjet Thruster
Characterisation of a Steady State MPD-Thruster with a Radiation Cooled Anode
Experimental Performance of a Low Power Neutralizer for a Micronewton FEEP Thruster
Recent Improvements of Numerical Methods for the Simulation of MPD Thruster Flow on Adaptive Meshes
Thrust Performance and Thermal Analysis of a Low Power Arcjet Thruster
An Experimental Research on a CW CO~2 Laser Thruster
Two New Spacecraft Architectures and Their Impacts on Electric Propulsion
Performance of an 8 kW Hall Thruster
Simple Estimation of the Performance of a Low Power Arcjet Thruster with Diatomic Gas as Propellant
A Method of Placing a Spacecraft on High Orbit
Advanced Electric Propulsion for RLV Launched Geosynchronous Spacecraft
Torque Control of Hall Propelled Small Spacecraft
One Millinewton FEEP Thruster Tests
A Study on Nozzle Flow Quality of Low Power Arcjet Thruster for Improvement of Propulsion Efficiency