☆ 4.6 Article

Modeling of a retarding potential analyzer and comparison with Express-A in-flight measurements

FRONTIERS IN PHYSICS (2022)

Related references

Note: Only part of the references are listed.

Article Engineering, Aerospace

Characterization of a high-power Hall thruster operation in direct-drive

Maryam Reza et al.

Summary: This paper presents in-depth investigations on the performance and controllability of a direct-drive Hall thruster system. Three different thruster control laws were implemented and proven effective in controlling the thruster behavior amidst varying solar array characteristics. The study revealed minimal differences in thruster performance parameters between direct-drive and conventional power supply, with a focus on the impact of grounding on thruster plume interaction with the spacecraft.

ACTA ASTRONAUTICA (2021)

Add to Collection

Article Physics, Fluids & Plasmas

Non-Maxwellian electron energy probability functions in the plume of a SPT-100 Hall thruster

G. Giono et al.

PLASMA SOURCES SCIENCE & TECHNOLOGY (2018)

Add to Collection

Article Physics, Fluids & Plasmas

Electrostatic Discharge Testing of Multijunction Solar Array Coupons After Combined Space Environmental Exposures

Kenneth H. Wright et al.

IEEE TRANSACTIONS ON PLASMA SCIENCE (2012)

Add to Collection

Article Mathematics, Applied

Numerical Study of Hall Thruster Plume and Sputtering Erosion

Li Yan et al.

JOURNAL OF APPLIED MATHEMATICS (2012)

Add to Collection

Article Physics, Applied

Anomalous conductivity and secondary electron emission in Hall effect thrusters

L. Garrigues et al.

JOURNAL OF APPLIED PHYSICS (2006)

Add to Collection

Article Engineering, Electrical & Electronic

Interaction of charged spacecraft with electric propulsion plume: On orbit data and ground test results

Justin J. Likar et al.

IEEE TRANSACTIONS ON NUCLEAR SCIENCE (2006)

Add to Collection

Article Engineering, Aerospace

SMART-1: An analysis of flight data

DM Di Cara et al.

ACTA ASTRONAUTICA (2005)

Add to Collection

Article Engineering, Aerospace

Plume modeling of stationary plasma thrusters and interactions with the Express-A spacecraft

IG Mikellides et al.

JOURNAL OF SPACECRAFT AND ROCKETS (2002)

Add to Collection

Article Engineering, Aerospace

Plume study of a 1.35-kW SPT-100 using an ExB probe

SW Kim et al.

JOURNAL OF SPACECRAFT AND ROCKETS (2002)

Add to Collection

Article Physics, Applied

Far field modeling of the plasma plume of a Hall thruster

ID Boyd et al.

JOURNAL OF APPLIED PHYSICS (2002)

Add to Collection

Article Physics, Fluids & Plasmas

Charged particle motion inside the retarding potential analyzer

CK Chao et al.

PHYSICS OF PLASMAS (2000)

Add to Collection

© Peeref 2019-2024. All rights reserved.