Results 71 to 80 of about 6,632 (182)

Performance and Facility Background Pressure Characterization Tests of NASAs 12.5-kW Hall Effect Rocket with Magnetic Shielding Thruster [PDF]

open access: yes
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

open access: yesApplied Sciences
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]

open access: yesSci Adv, 2022
Zolotukhin DB   +4 more
europepmc   +1 more source

Effect of Background Pressure on the Plasma Oscillation Characteristics of the HiVHAc Hall Thruster [PDF]

open access: yes
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]

open access: yesКосмические аппараты и технологии
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  

An Analysis of the Effect of Hall Thruster Plumes on Surface Charging of a Complex Spacecraft Structure

open access: yesApplied Sciences
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 thruster technology [PDF]

open access: yes
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]

open access: yesSci Rep, 2021
Zheng J   +17 more
europepmc   +1 more source

13kW Advanced Electric Propulsion Flight System Development and Qualification [PDF]

open access: yes
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

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