Plasma Sheath around Chandrayaan-3 Landing Site: A Case Study

India’s lander-rover mission Chandrayaan-3 is scheduled to be launched in mid-2023. We have simulated a realistic scenario and investigated the electric potential development over the Chandrayaan-3 landing site under the influence of observed solar ultraviolet/extreme-ultraviolet radiation and real...

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Main Authors: Trinesh Sana, S. K. Mishra
Format: Article
Language:English
Published: IOP Publishing 2023-01-01
Series:The Planetary Science Journal
Subjects:
Online Access:https://doi.org/10.3847/PSJ/acf1a1
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author Trinesh Sana
S. K. Mishra
author_facet Trinesh Sana
S. K. Mishra
author_sort Trinesh Sana
collection DOAJ
description India’s lander-rover mission Chandrayaan-3 is scheduled to be launched in mid-2023. We have simulated a realistic scenario and investigated the electric potential development over the Chandrayaan-3 landing site under the influence of observed solar ultraviolet/extreme-ultraviolet radiation and real plasma parameters measured by THEMIS as a case study. The electric potential structures have been derived by solving Poisson’s equation, which is coupled with latitude-dependent fermionic photoelectrons, non-Maxwellian plasma electrons, and cold ions. A dynamic variation of the potential structure around the sunlit landing site has been observed through the analysis. This study predicts a photoelectron density range from 10 to 40 cm ^−3 and mean energy range from 2.6 to 3 eV near the surface of the Chandrayaan-3 landing site, which may be tested by the in situ measurement.
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spelling doaj.art-56d661fef4db49dab40be079d5d939812024-02-03T12:16:42ZengIOP PublishingThe Planetary Science Journal2632-33382023-01-014915810.3847/PSJ/acf1a1Plasma Sheath around Chandrayaan-3 Landing Site: A Case StudyTrinesh Sana0https://orcid.org/0000-0001-8070-139XS. K. Mishra1https://orcid.org/0000-0002-2446-4032Physical Research Laboratory, Ahmedabad , Gujarat 380009, India ; sanatrinesh@gmail.com; Indian Institute of Technology Gandhinagar, Gandhinagar, Gujarat 382055, IndiaPhysical Research Laboratory, Ahmedabad , Gujarat 380009, India ; sanatrinesh@gmail.comIndia’s lander-rover mission Chandrayaan-3 is scheduled to be launched in mid-2023. We have simulated a realistic scenario and investigated the electric potential development over the Chandrayaan-3 landing site under the influence of observed solar ultraviolet/extreme-ultraviolet radiation and real plasma parameters measured by THEMIS as a case study. The electric potential structures have been derived by solving Poisson’s equation, which is coupled with latitude-dependent fermionic photoelectrons, non-Maxwellian plasma electrons, and cold ions. A dynamic variation of the potential structure around the sunlit landing site has been observed through the analysis. This study predicts a photoelectron density range from 10 to 40 cm ^−3 and mean energy range from 2.6 to 3 eV near the surface of the Chandrayaan-3 landing site, which may be tested by the in situ measurement.https://doi.org/10.3847/PSJ/acf1a1Space plasmasSolar windThe Moon
spellingShingle Trinesh Sana
S. K. Mishra
Plasma Sheath around Chandrayaan-3 Landing Site: A Case Study
The Planetary Science Journal
Space plasmas
Solar wind
The Moon
title Plasma Sheath around Chandrayaan-3 Landing Site: A Case Study
title_full Plasma Sheath around Chandrayaan-3 Landing Site: A Case Study
title_fullStr Plasma Sheath around Chandrayaan-3 Landing Site: A Case Study
title_full_unstemmed Plasma Sheath around Chandrayaan-3 Landing Site: A Case Study
title_short Plasma Sheath around Chandrayaan-3 Landing Site: A Case Study
title_sort plasma sheath around chandrayaan 3 landing site a case study
topic Space plasmas
Solar wind
The Moon
url https://doi.org/10.3847/PSJ/acf1a1
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AT skmishra plasmasheatharoundchandrayaan3landingsiteacasestudy