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Development of low cost double probe plasma measurement system for a lean satellite HORYU-IV

Development of low cost double probe plasma measurement system for a lean satellite HORYU-IV
Development of low cost double probe plasma measurement system for a lean satellite HORYU-IV
A lean satellite is equivalent to a small/micro/nano/pico satellite that utilizes untraditional risk-taking development approaches to achieve low-cost and fast-delivery. Lean satellites have demonstrated great ability to be used for the study of space plasma and Earth’s ionosphere which has helped in the prediction of many astrophysical phenomena and forecasting of geophysical changes on ground. Several methods have been employed in the measurement of space plasma parameters over the years using the Langmuir Probe. These methods employed different techniques using single probes or double probes. Single probe requires a well-defined reference which is difficult in small spacecraft. Moreover, high current flow in the saturation mode may destroy the probe and on-board circuitry. A low cost double Langmuir probe made of gold with its measurement circuit has been designed and tested inside RF generated Argon plasma in the pressure of 1.4×10-2 Pa that confirms the electron density from 1010 to 1012 m-3. Important design considerations such as operability of the designed system in low earth orbit grade plasma, mitigation of probe contamination and sputtering of the electrode surface were analysed in the paper to ensure that the developed system can provide high fidelity plasma measurement data throughout the life span of HORYU-IV (Arc Event Generator and Investigator Satellite) which is a 13 kg, 40 cm cubic lean satellite under development at the Kyushu Institute of Technology.
1884-0485
Tejumola, TAIWO RAPHAEL
1694d442-f900-48b6-9c17-ba66185ecd4c
Tanaka, Atomu
4620cac7-1c80-410a-99ef-4824c6df5ee0
Khan, Arifur
ecb240c5-deb7-4a28-8a25-875d0c8e041b
Cho, Mengu
74e2e375-1bb1-4adc-8c90-539206caed66
others,
00f5cf31-baf4-46f0-ac82-5e61bb65d0dd
Tejumola, TAIWO RAPHAEL
1694d442-f900-48b6-9c17-ba66185ecd4c
Tanaka, Atomu
4620cac7-1c80-410a-99ef-4824c6df5ee0
Khan, Arifur
ecb240c5-deb7-4a28-8a25-875d0c8e041b
Cho, Mengu
74e2e375-1bb1-4adc-8c90-539206caed66
others,
00f5cf31-baf4-46f0-ac82-5e61bb65d0dd

Tejumola, TAIWO RAPHAEL, Tanaka, Atomu, Khan, Arifur, Cho, Mengu and others, (2016) Development of low cost double probe plasma measurement system for a lean satellite HORYU-IV. Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, 14. (doi:10.2322/tastj.14.Pr_39).

Record type: Article

Abstract

A lean satellite is equivalent to a small/micro/nano/pico satellite that utilizes untraditional risk-taking development approaches to achieve low-cost and fast-delivery. Lean satellites have demonstrated great ability to be used for the study of space plasma and Earth’s ionosphere which has helped in the prediction of many astrophysical phenomena and forecasting of geophysical changes on ground. Several methods have been employed in the measurement of space plasma parameters over the years using the Langmuir Probe. These methods employed different techniques using single probes or double probes. Single probe requires a well-defined reference which is difficult in small spacecraft. Moreover, high current flow in the saturation mode may destroy the probe and on-board circuitry. A low cost double Langmuir probe made of gold with its measurement circuit has been designed and tested inside RF generated Argon plasma in the pressure of 1.4×10-2 Pa that confirms the electron density from 1010 to 1012 m-3. Important design considerations such as operability of the designed system in low earth orbit grade plasma, mitigation of probe contamination and sputtering of the electrode surface were analysed in the paper to ensure that the developed system can provide high fidelity plasma measurement data throughout the life span of HORYU-IV (Arc Event Generator and Investigator Satellite) which is a 13 kg, 40 cm cubic lean satellite under development at the Kyushu Institute of Technology.

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Published date: November 2016

Identifiers

Local EPrints ID: 498232
URI: http://eprints.soton.ac.uk/id/eprint/498232
ISSN: 1884-0485
PURE UUID: d85baa28-58a8-4086-8893-289af25447d8
ORCID for TAIWO RAPHAEL Tejumola: ORCID iD orcid.org/0000-0002-2918-1533

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Date deposited: 12 Feb 2025 17:50
Last modified: 22 Aug 2025 02:43

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Author: TAIWO RAPHAEL Tejumola ORCID iD
Author: Atomu Tanaka
Author: Arifur Khan
Author: Mengu Cho
Author: others

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