Numerical Analysis of Ground Testing for the Intake Device of an Atmosphere-Breathing Electric Propulsion

Fuente: arXiv
Salvato in:
Dettagli Bibliografici
Autori principali: Moon, Geonwoong, Jun, Eunji, Yi, Minwoo, Choi, Hyunjin, Park, Kangmin, Kim, Younho, Lee, Jaecheong, Lee, Jeongjae, Joo, Gahee, Shin, Seungho, Lee, Se, Jeong, Yunhwang
Natura: Preprint
Pubblicazione: 2025
Soggetti:
Accesso online:
Tags: Aggiungi Tag
Nessun Tag, puoi essere il primo ad aggiungerne!!
_version_ 1866912599107436544
author Moon, Geonwoong
Jun, Eunji
Yi, Minwoo
Choi, Hyunjin
Park, Kangmin
Kim, Younho
Lee, Jaecheong
Lee, Jeongjae
Joo, Gahee
Shin, Seungho
Lee, Se
Jeong, Yunhwang
author_facet Moon, Geonwoong
Jun, Eunji
Yi, Minwoo
Choi, Hyunjin
Park, Kangmin
Kim, Younho
Lee, Jaecheong
Lee, Jeongjae
Joo, Gahee
Shin, Seungho
Lee, Se
Jeong, Yunhwang
contents Atmosphere-breathing electric propulsion (ABEP) is a promising technology for long-term orbit maintenance in very-low-Earth orbit. The intake device plays a crucial role in capturing and supplying propellant, and its capture efficiency is a key indicator of drag-compensation feasibility. For experimental evaluation, an electric-propulsion (EP) plasma plume can be used as a particle-flow generator to simulate the VLEO atmosphere in ground facilities. This study numerically investigates the interaction of an EP plasma plume with an intake device to establish guidelines for measuring capture efficiency in conventional vacuum facilities. A hybrid PIC-DSMC method with ion-surface interaction models is employed to simulate the plasma plume incident on the intake. The composition of the captured flow is governed by beam-ion energy and species mass: lowering the energy and using lighter atmospheric constituents increase plume divergence and promote neutralization, yielding a neutral-dominated outlet flow. Sputtering of the intake surface becomes non-negligible at high energies but can be mitigated by operating at appropriately low beam energies. The results show that simultaneous ion and neutral diagnostics are required for reliable capture-efficiency evaluation when using EP plasma plumes in ground facilities.
format Preprint
id arxiv_https___arxiv_org_abs_2509_17547
institution arXiv
publishDate 2025
record_format arxiv
spellingShingle Numerical Analysis of Ground Testing for the Intake Device of an Atmosphere-Breathing Electric Propulsion
Moon, Geonwoong
Jun, Eunji
Yi, Minwoo
Choi, Hyunjin
Park, Kangmin
Kim, Younho
Lee, Jaecheong
Lee, Jeongjae
Joo, Gahee
Shin, Seungho
Lee, Se
Jeong, Yunhwang
Plasma Physics
Atmosphere-breathing electric propulsion (ABEP) is a promising technology for long-term orbit maintenance in very-low-Earth orbit. The intake device plays a crucial role in capturing and supplying propellant, and its capture efficiency is a key indicator of drag-compensation feasibility. For experimental evaluation, an electric-propulsion (EP) plasma plume can be used as a particle-flow generator to simulate the VLEO atmosphere in ground facilities. This study numerically investigates the interaction of an EP plasma plume with an intake device to establish guidelines for measuring capture efficiency in conventional vacuum facilities. A hybrid PIC-DSMC method with ion-surface interaction models is employed to simulate the plasma plume incident on the intake. The composition of the captured flow is governed by beam-ion energy and species mass: lowering the energy and using lighter atmospheric constituents increase plume divergence and promote neutralization, yielding a neutral-dominated outlet flow. Sputtering of the intake surface becomes non-negligible at high energies but can be mitigated by operating at appropriately low beam energies. The results show that simultaneous ion and neutral diagnostics are required for reliable capture-efficiency evaluation when using EP plasma plumes in ground facilities.
title Numerical Analysis of Ground Testing for the Intake Device of an Atmosphere-Breathing Electric Propulsion
topic Plasma Physics
url https://arxiv.org/abs/2509.17547