Design of an energy absorption system for the landing of space exploration modules

Design of an energy absorption system for the landing of space exploration modules

Currently, space exploration is becoming an increasingly important activity since it allows increased knowledge regarding the formation of planets, economic activities (space mining) as well as a better understanding of geological and biological phenomena that allow the creation of space in the futu...

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Egile Nagusiak: Estrada-Barbosa , Quirino, Martínez-Rayón, Eladio, Reynoso-Jardón, Elva Lilia, Silva-Aceves, Jesús, Nandayapa-Alfaro, Manuel de Jesús, Wiebe, Lara C., Enríquez-Aguilera, Francisco Javier
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Argitaratua: Universidad Autónoma de Baja California 2024
Sarrera elektronikoa:https://recit.uabc.mx/index.php/revista/article/view/345
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spelling recit-article-3452024-05-23T18:56:42Z Design of an energy absorption system for the landing of space exploration modules Diseño de un sistema de absorción de energía para el aterrizaje de módulos de exploración espacial Estrada-Barbosa , Quirino Martínez-Rayón, Eladio Reynoso-Jardón, Elva Lilia Silva-Aceves, Jesús Nandayapa-Alfaro, Manuel de Jesús Wiebe, Lara C. Enríquez-Aguilera, Francisco Javier Thin-walled structure Space exploration Finite element method Energy absorption system Estructura de pared delgada Exploración espacial Método de elemento finito Sistema de absorción de energía Currently, space exploration is becoming an increasingly important activity since it allows increased knowledge regarding the formation of planets, economic activities (space mining) as well as a better understanding of geological and biological phenomena that allow the creation of space in the future of human habitats outside planet Earth. In this sense, one of the main problems of space exploration is associated with the safe landing of space probes. Based on the above, this article proposes the design of a passive type of energy absorption system based on plastic deformation of aluminum structural profiles. For this purpose, structural profiles with various geometric shapes were individually designed and evaluated using the Abaqus finite element software. The numerical evaluation was carried out through compression tests in conjunction with the calculation of the main impact resistance parameters. The results showed a better performance of the HSC-1 profile which obtained the best crushing force efficiency (CH-C) equal to 0.83. From the above, it was implemented in a discrete model of a generic space lander. Actualmente la exploración espacial está convirtiéndose en una actividad cada vez más importante desde que permiten aumentar el conocimiento en cuanto a la formación de planetas, actividades económicas (minería espacial) así como un mejor entendimiento de fenómenos geológicos y biológicos que permitan en el futuro la creación de hábitats humanos fuera del planeta Tierra. En este sentido, uno de los principales problemas de la exploración espacial está asociado al aterrizaje seguro de las sondas espaciales. A partir de lo anterior el presente artículo propone el diseño de un sistema de absorción de energía del tipo pasivo basado en deformación plástica de perfiles estructurales de aluminio. Para tal propósito se diseñaron y evaluaron individualmente perfiles estructurales con diversas formas geométricas utilizando el software de elementos finitos Abaqus. La evaluación numérica se realizó a través de ensayos de compresión en conjunto con el cálculo de los principales parámetros de resistencia al impacto. Los resultados mostraron un mejor desempeño del perfil CH-C el cual obtuvo la mejor eficiencia de fuerza de aplastamiento (CFE) igual a 0.83. A partir de lo anterior se implementó en un modelo discreto de un módulo de aterrizaje. Universidad Autónoma de Baja California 2024-04-15 info:eu-repo/semantics/article info:eu-repo/semantics/publishedVersion application/pdf text/html application/zip https://recit.uabc.mx/index.php/revista/article/view/345 10.37636/recit.v7n2e345 REVISTA DE CIENCIAS TECNOLÓGICAS; Vol. 7 No. 2 (2024): April-June; e345 REVISTA DE CIENCIAS TECNOLÓGICAS; Vol. 7 Núm. 2 (2024): Abril-Junio; e345 2594-1925 spa https://recit.uabc.mx/index.php/revista/article/view/345/555 https://recit.uabc.mx/index.php/revista/article/view/345/556 https://recit.uabc.mx/index.php/revista/article/view/345/557 Copyright (c) 2024 Quirino Estrada-Barbosa , Eladio Martínez-Rayón, Elva Lilia Reynoso-Jardón, Jesús Silva-Aceves, Manuel de Jesús Nandayapa-Alfaro, Lara C. Wiebe, Francisco Javier Enríquez-Aguilera https://creativecommons.org/licenses/by/4.0
institution RECIT
collection OJS
language spa
format Online
author Estrada-Barbosa , Quirino
Martínez-Rayón, Eladio
Reynoso-Jardón, Elva Lilia
Silva-Aceves, Jesús
Nandayapa-Alfaro, Manuel de Jesús
Wiebe, Lara C.
Enríquez-Aguilera, Francisco Javier
spellingShingle Estrada-Barbosa , Quirino
Martínez-Rayón, Eladio
Reynoso-Jardón, Elva Lilia
Silva-Aceves, Jesús
Nandayapa-Alfaro, Manuel de Jesús
Wiebe, Lara C.
Enríquez-Aguilera, Francisco Javier
Design of an energy absorption system for the landing of space exploration modules
author_facet Estrada-Barbosa , Quirino
Martínez-Rayón, Eladio
Reynoso-Jardón, Elva Lilia
Silva-Aceves, Jesús
Nandayapa-Alfaro, Manuel de Jesús
Wiebe, Lara C.
Enríquez-Aguilera, Francisco Javier
author_sort Estrada-Barbosa , Quirino
title Design of an energy absorption system for the landing of space exploration modules
title_short Design of an energy absorption system for the landing of space exploration modules
title_full Design of an energy absorption system for the landing of space exploration modules
title_fullStr Design of an energy absorption system for the landing of space exploration modules
title_full_unstemmed Design of an energy absorption system for the landing of space exploration modules
title_sort design of an energy absorption system for the landing of space exploration modules
description Currently, space exploration is becoming an increasingly important activity since it allows increased knowledge regarding the formation of planets, economic activities (space mining) as well as a better understanding of geological and biological phenomena that allow the creation of space in the future of human habitats outside planet Earth. In this sense, one of the main problems of space exploration is associated with the safe landing of space probes. Based on the above, this article proposes the design of a passive type of energy absorption system based on plastic deformation of aluminum structural profiles. For this purpose, structural profiles with various geometric shapes were individually designed and evaluated using the Abaqus finite element software. The numerical evaluation was carried out through compression tests in conjunction with the calculation of the main impact resistance parameters. The results showed a better performance of the HSC-1 profile which obtained the best crushing force efficiency (CH-C) equal to 0.83. From the above, it was implemented in a discrete model of a generic space lander.
publisher Universidad Autónoma de Baja California
publishDate 2024
url https://recit.uabc.mx/index.php/revista/article/view/345
_version_ 1808123086573142016

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