The IPG6-B as a research facility to support future development of electric propulsion
Raumfahrtrelevante Plasmen und deren anwendungsbezogene Klassifizierung
Experimental study on the performance characteristics of a miniature microwave discharge cathode
Investigation on operational stability of a pulsed plasma thruster with a pressure probe
Investigation of the Plasma Current Density of a Pulsed Plasma Thruster
Wall Ion Loss Reduction by Acceleration Zone Shifting in Anode-Layer Hall Thruster
Heterogeneous Catalysis Models of High-Temperature Materials in High-Enthalpy Flows
Investigation of the Magnetic Field in a Pulsed Plasma Thruster
Propellant Utilization Efficiency in a Pulsed Plasma Thruster
Experimental Methodology to Assess Atomic Recombination on High-Temperature Materials