Skip to Main content Skip to Navigation
Journal articles

Multi-Objective Multidisciplinary Design Optimization Approach for Partially Reusable Launch Vehicle Design

Loic Brevault 1 Mathieu Balesdent 1 Ali Hebbal 1, 2
2 BONUS - Optimisation de grande taille et calcul large échelle
Inria Lille - Nord Europe, CRIStAL - Centre de Recherche en Informatique, Signal et Automatique de Lille - UMR 9189
Abstract : Reusability of the first stage of launch vehicles may offer new perspectives to lower the cost of payload injection into orbit if sufficient reliability and efficient refurbishment can be achieved. One possible option that may be explored is to design the vehicle first stage for both reusable and expendable uses, in order to increase the flexibility and adaptability to different target missions. This paper proposes a multilevel multidisciplinary design optimization (MDO) approach to design aerospace vehicles addressing multimission problems. The proposed approach is focused on the design of a family of launchers for different missions sharing commonalities using multi-objective MDO to account for the computational cost associated with the discipline simulations. The multimission problem addressed considers two missions: 1) a reusable configuration for a sun synchronous orbit with a medium payload range and recovery of the first stage using a gliding-back strategy; 2) an expendable configuration for a medium payload injected into a geostationary transfer orbit. A dedicated MDO formulation introducing couplings between the missions is proposed in order to efficiently solve such a coupled problem while limiting the number of calls to the exact multidisciplinary analysis thanks to the use of Gaussian processes and multi-objective efficient global optimization.
Document type :
Journal articles
Complete list of metadata

https://hal.archives-ouvertes.fr/hal-03046307
Contributor : Ali Hebbal Connect in order to contact the contributor
Submitted on : Thursday, April 8, 2021 - 5:31:10 PM
Last modification on : Tuesday, January 4, 2022 - 6:14:27 AM

File

Dtis21053 post print.pdf
Files produced by the author(s)

Identifiers

Citation

Loic Brevault, Mathieu Balesdent, Ali Hebbal. Multi-Objective Multidisciplinary Design Optimization Approach for Partially Reusable Launch Vehicle Design. Journal of Spacecraft and Rockets, American Institute of Aeronautics and Astronautics, 2020, 57 (2), pp.373-390. ⟨10.2514/1.A34601⟩. ⟨hal-03046307⟩

Share

Metrics

Les métriques sont temporairement indisponibles