Multi-objective design optimization and physics-based sensitivity analysis of field emission electric propulsion for CubeSat platforms-Reference-Cited by-同舟云学术

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Multi-objective design optimization and physics-based sensitivity analysis of field emission electric propulsion for CubeSat platforms

Published:2024-11 Issue: Volume:154 Page:109516
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Yeo Suk Hyun^ORCID,Gadisa Dinaol^ORCID,Ogawa Hideaki^ORCID,Bang HyoChoong^ORCID

Funder

Japan Society for the Promotion of Science

Korea Ministry of Science and ICT

Publisher

Elsevier BV

Reference62 articles.

1. Direct thrust test and asymmetric performance of porous ionic liquid electrospray thruster;Guo;Chin. J. Aeronaut.,2023

2. CubeSat evolution: analyzing CubeSat capabilities for conducting science missions;Poghosyan;Prog. Aerosp. Sci.,2017

3. Fundamentals of Electric Propulsion: Ion and Hall Thrusters;Dan M,2008

4. Modeling and Parametric Performance Analysis of Field Emission Electric Propulsion;Dinaol,2023

5. Performance and lifetime testing of a pulsed plasma thruster for cubesat applications;Ciaralli;Aerosp. Sci. Technol.,2015

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