A Multidisciplinary Optimization Framework for Ecodesign of Reusable Microsatellite Launchers

The commercial space launch sector is currently undergoing a significant shift, with increasing competition and demand for launch services, as well as growing concerns about the environmental impact of rocket launches. To address these challenges, within the New Space Portugal project scope, a multi...

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Main Authors: Girolamo Musso, Iara Figueiras, Héléna Goubel, Afonso Gonçalves, Ana Laura Costa, Bruna Ferreira, Lara Azeitona, Simão Barata, Alain Souza, Frederico Afonso, Inês Ribeiro, Fernando Lau
Format: Article
Language:English
Published: MDPI AG 2024-01-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/11/2/126
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author Girolamo Musso
Iara Figueiras
Héléna Goubel
Afonso Gonçalves
Ana Laura Costa
Bruna Ferreira
Lara Azeitona
Simão Barata
Alain Souza
Frederico Afonso
Inês Ribeiro
Fernando Lau
author_facet Girolamo Musso
Iara Figueiras
Héléna Goubel
Afonso Gonçalves
Ana Laura Costa
Bruna Ferreira
Lara Azeitona
Simão Barata
Alain Souza
Frederico Afonso
Inês Ribeiro
Fernando Lau
author_sort Girolamo Musso
collection DOAJ
description The commercial space launch sector is currently undergoing a significant shift, with increasing competition and demand for launch services, as well as growing concerns about the environmental impact of rocket launches. To address these challenges, within the New Space Portugal project scope, a multidisciplinary framework for designing and optimizing new launch vehicles is proposed. Creating a more resilient and responsible space industry can be achieved by combining technological innovation and environmental sustainability, as emphasized by the framework. The main scope of the framework was to couple all the disciplines relevant to the space vehicle design in a modular way. Significant emphasis was placed on the infusion of ecodesign principles, including Life Cycle Assessment (LCA) considerations. Optimization techniques were employed to enhance the design and help designers conduct trade-off studies. In general, this multidisciplinary framework aims to provide a comprehensive approach to designing next-generation launch vehicles that meet the demands of a rapidly changing market while also minimizing their environmental impact. A methodology that leverages the strengths of both genetic and gradient-based algorithms is employed for optimizations with the objectives of maximizing the apogee altitude and minimizing the Global Warming Potential (GWP). Despite only being tested at the moment for sounding rockets, the framework has demonstrated promising results. It has illuminated the potential of this approach, leading to the identification of three optimal designs: one for maximizing the apogee, another for minimizing GWP, and a compromise design that strikes a balance between the two objectives. The outcomes yielded a maximum apogee of <inline-formula><math xmlns="http://www.w3.org/1998/Math/MathML" display="inline"><semantics><mrow><mn>6.41</mn></mrow></semantics></math></inline-formula> km, a minimum GWP of <inline-formula><math xmlns="http://www.w3.org/1998/Math/MathML" display="inline"><semantics><mrow><mn>9.06</mn></mrow></semantics></math></inline-formula> kg <inline-formula><math xmlns="http://www.w3.org/1998/Math/MathML" display="inline"><semantics><msub><mrow><mi>CO</mi></mrow><mrow><msub><mn>2</mn><mrow><mi>e</mi><mi>q</mi></mrow></msub></mrow></msub></semantics></math></inline-formula>, and a balanced compromise design featuring an apogee of <inline-formula><math xmlns="http://www.w3.org/1998/Math/MathML" display="inline"><semantics><mrow><mn>5.75</mn></mrow></semantics></math></inline-formula> km and a GWP of <inline-formula><math xmlns="http://www.w3.org/1998/Math/MathML" display="inline"><semantics><mrow><mn>25.64</mn></mrow></semantics></math></inline-formula> kg <inline-formula><math xmlns="http://www.w3.org/1998/Math/MathML" display="inline"><semantics><msub><mrow><mi>CO</mi></mrow><mrow><msub><mn>2</mn><mrow><mi>e</mi><mi>q</mi></mrow></msub></mrow></msub></semantics></math></inline-formula>.
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spelling doaj.art-6f350be074814c8da9c29c60d0d3cbea2024-02-23T15:03:19ZengMDPI AGAerospace2226-43102024-01-0111212610.3390/aerospace11020126A Multidisciplinary Optimization Framework for Ecodesign of Reusable Microsatellite LaunchersGirolamo Musso0Iara Figueiras1Héléna Goubel2Afonso Gonçalves3Ana Laura Costa4Bruna Ferreira5Lara Azeitona6Simão Barata7Alain Souza8Frederico Afonso9Inês Ribeiro10Fernando Lau11IDMEC, Instituto Superior Técnico, Universidade de Lisboa, Av. Rovisco Pais, No. 1, 1049-001 Lisbon, PortugalIDMEC, Instituto Superior Técnico, Universidade de Lisboa, Av. Rovisco Pais, No. 1, 1049-001 Lisbon, PortugalIDMEC, Instituto Superior Técnico, Universidade de Lisboa, Av. Rovisco Pais, No. 1, 1049-001 Lisbon, PortugalIDMEC, Instituto Superior Técnico, Universidade de Lisboa, Av. Rovisco Pais, No. 1, 1049-001 Lisbon, PortugalIDMEC, Instituto Superior Técnico, Universidade de Lisboa, Av. Rovisco Pais, No. 1, 1049-001 Lisbon, PortugalIDMEC, Instituto Superior Técnico, Universidade de Lisboa, Av. Rovisco Pais, No. 1, 1049-001 Lisbon, PortugalIDMEC, Instituto Superior Técnico, Universidade de Lisboa, Av. Rovisco Pais, No. 1, 1049-001 Lisbon, PortugalIDMEC, Instituto Superior Técnico, Universidade de Lisboa, Av. Rovisco Pais, No. 1, 1049-001 Lisbon, PortugalIDMEC, Instituto Superior Técnico, Universidade de Lisboa, Av. Rovisco Pais, No. 1, 1049-001 Lisbon, PortugalIDMEC, Instituto Superior Técnico, Universidade de Lisboa, Av. Rovisco Pais, No. 1, 1049-001 Lisbon, PortugalIDMEC, Instituto Superior Técnico, Universidade de Lisboa, Av. Rovisco Pais, No. 1, 1049-001 Lisbon, PortugalIDMEC, Instituto Superior Técnico, Universidade de Lisboa, Av. Rovisco Pais, No. 1, 1049-001 Lisbon, PortugalThe commercial space launch sector is currently undergoing a significant shift, with increasing competition and demand for launch services, as well as growing concerns about the environmental impact of rocket launches. To address these challenges, within the New Space Portugal project scope, a multidisciplinary framework for designing and optimizing new launch vehicles is proposed. Creating a more resilient and responsible space industry can be achieved by combining technological innovation and environmental sustainability, as emphasized by the framework. The main scope of the framework was to couple all the disciplines relevant to the space vehicle design in a modular way. Significant emphasis was placed on the infusion of ecodesign principles, including Life Cycle Assessment (LCA) considerations. Optimization techniques were employed to enhance the design and help designers conduct trade-off studies. In general, this multidisciplinary framework aims to provide a comprehensive approach to designing next-generation launch vehicles that meet the demands of a rapidly changing market while also minimizing their environmental impact. A methodology that leverages the strengths of both genetic and gradient-based algorithms is employed for optimizations with the objectives of maximizing the apogee altitude and minimizing the Global Warming Potential (GWP). Despite only being tested at the moment for sounding rockets, the framework has demonstrated promising results. It has illuminated the potential of this approach, leading to the identification of three optimal designs: one for maximizing the apogee, another for minimizing GWP, and a compromise design that strikes a balance between the two objectives. The outcomes yielded a maximum apogee of <inline-formula><math xmlns="http://www.w3.org/1998/Math/MathML" display="inline"><semantics><mrow><mn>6.41</mn></mrow></semantics></math></inline-formula> km, a minimum GWP of <inline-formula><math xmlns="http://www.w3.org/1998/Math/MathML" display="inline"><semantics><mrow><mn>9.06</mn></mrow></semantics></math></inline-formula> kg <inline-formula><math xmlns="http://www.w3.org/1998/Math/MathML" display="inline"><semantics><msub><mrow><mi>CO</mi></mrow><mrow><msub><mn>2</mn><mrow><mi>e</mi><mi>q</mi></mrow></msub></mrow></msub></semantics></math></inline-formula>, and a balanced compromise design featuring an apogee of <inline-formula><math xmlns="http://www.w3.org/1998/Math/MathML" display="inline"><semantics><mrow><mn>5.75</mn></mrow></semantics></math></inline-formula> km and a GWP of <inline-formula><math xmlns="http://www.w3.org/1998/Math/MathML" display="inline"><semantics><mrow><mn>25.64</mn></mrow></semantics></math></inline-formula> kg <inline-formula><math xmlns="http://www.w3.org/1998/Math/MathML" display="inline"><semantics><msub><mrow><mi>CO</mi></mrow><mrow><msub><mn>2</mn><mrow><mi>e</mi><mi>q</mi></mrow></msub></mrow></msub></semantics></math></inline-formula>.https://www.mdpi.com/2226-4310/11/2/126Multidisciplinary Design Optimizationmicrosatellite launcherssustainabilityLife Cycle AssessmentecodesignNew Space Portugal
spellingShingle Girolamo Musso
Iara Figueiras
Héléna Goubel
Afonso Gonçalves
Ana Laura Costa
Bruna Ferreira
Lara Azeitona
Simão Barata
Alain Souza
Frederico Afonso
Inês Ribeiro
Fernando Lau
A Multidisciplinary Optimization Framework for Ecodesign of Reusable Microsatellite Launchers
Aerospace
Multidisciplinary Design Optimization
microsatellite launchers
sustainability
Life Cycle Assessment
ecodesign
New Space Portugal
title A Multidisciplinary Optimization Framework for Ecodesign of Reusable Microsatellite Launchers
title_full A Multidisciplinary Optimization Framework for Ecodesign of Reusable Microsatellite Launchers
title_fullStr A Multidisciplinary Optimization Framework for Ecodesign of Reusable Microsatellite Launchers
title_full_unstemmed A Multidisciplinary Optimization Framework for Ecodesign of Reusable Microsatellite Launchers
title_short A Multidisciplinary Optimization Framework for Ecodesign of Reusable Microsatellite Launchers
title_sort multidisciplinary optimization framework for ecodesign of reusable microsatellite launchers
topic Multidisciplinary Design Optimization
microsatellite launchers
sustainability
Life Cycle Assessment
ecodesign
New Space Portugal
url https://www.mdpi.com/2226-4310/11/2/126
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