Study on inversion method of wall erosion information of on-orbit Hall thruster based on low-frequency oscillation signals and neural networks. [PDF]
Han K +7 more
europepmc +1 more source
Performance and Facility Background Pressure Characterization Tests of NASAs 12.5-kW Hall Effect Rocket with Magnetic Shielding Thruster [PDF]
NASA's Space Technology Mission Directorate (STMD) Solar Electric Propulsion Technology Demonstration Mission (SEP/TDM) project is funding the development of a 12.5-kW Hall thruster system to support future NASA missions.
Haag, Thomas +12 more
core +1 more source
Interplanetary Mission Performance Assessment of a TANDEM Electric Thruster-Based Spacecraft
The aim of this paper is to analyze the transfer performance of a spacecraft equipped with a TANDEM electric propulsion system in a classical interplanetary mission scenario targeting Mars, Venus, or a near-Earth asteroid. The TANDEM concept is a coaxial,
Alessandro A. Quarta
doaj +1 more source
Demonstration of electric micropropulsion multimodality. [PDF]
Zolotukhin DB +4 more
europepmc +1 more source
Effect of Background Pressure on the Plasma Oscillation Characteristics of the HiVHAc Hall Thruster [PDF]
During a component compatibility test of the NASA HiVHAc Hall thruster, a number of plasma diagnostics were implemented to study the effect of varying facility background pressure on thruster operation.
Brown, Daniel L. +3 more
core +1 more source
Development and implementation of promising technologies in JSC EDB Fakel [PDF]
The enterprise is mastering a number of technologies for obtaining functional materials for monopropellant thruster and Hall-effect thruster. The article describes advances in the development of a catalyst for the decomposition of hydrazine with high ...
E. A. Bogdanova +2 more
doaj
This article aims to conduct an in-depth investigation into the environmental impact of Hall thruster plumes on spacecraft surface charging. The non-uniform plasma plume generated by Hall thrusters may trigger charging and discharging effects, making the
Xin Zhang +11 more
doaj +1 more source
MPD (MagnetoPlasmaDynamic) thrusters demonstrated between 2000 and 7000 seconds specific impulse at efficiencies approaching 40 percent, and were operated continuously at power levels over 500 kW.
Lapointe, Michael R. +2 more
core +1 more source
Integrated study on the comprehensive magnetic-field configuration performance in the 150 kW superconducting magnetoplasmadynamic thruster. [PDF]
Zheng J +17 more
europepmc +1 more source
13kW Advanced Electric Propulsion Flight System Development and Qualification [PDF]
The next phase of robotic and human deep space exploration missions requires high performance, high power solar electric propulsion systems for large-scale science missions and cargo transportation.
Barber, Matthew +6 more
core +1 more source

