Multi fidelity, multi-disciplinary optimisation for sustainable rocket-based launcher systems

Problem Definition:
Linking trajectory optimisation with disciplinary-specific numerical tools can result in numerical system that cannot be defined by ordinary differential equations, and are differential-algebraic systems (DAE). This is the case with shape deformation, aeroelasticity, structural deformation or surface ablation mixed with flight dynamics and optimal control. Multi-fidelity management within a multi-objective constrained closed system design optimisation can allow a highly complex system and environment to be more accurately modelled and simulated, accounting the interactions between all sub-systems balanced with practical limitations of computational efficiency.

Research Objectives:
Development of effective methods for integrating dynamic shape geometries into numerical solvers for PDAE (algebraic, ordinary and partial differential equations) systems
Integration and advancement of multi-fidelity management within design optimisation and propagation tools for trans-atmospheric flight systems
Application to multi-stage launch, ascent, orbital insertion and demise

Expected Results:
Tools to generate optimal sets of launch vehicle designs and mission designs for sustainability, including robustness, emissions, and debris generation (risk)
Assessment of the environmental impact at a system level of key parameters during early design phases
Assessments of different launch systems to inform LCA

Secondments:
Politecnico di Torino (POLITO, Torino, Italy, ca. 3 months): development/incorporation of propulsion and emissions modelling
Deimos Engineering and Systems SLU (DEIMOS, Puertollano, Spain, ca. 3 months): high/low fidelity model cross-validation

Benefits:
You will be working within our international group of > 30 researchers with experience in a broad range of sciences.
You will get in contact with the other members of this international consortium.
You will benefit from the well-structured training program offered by the host institution and the SLICE consortium to develop skills and thorough understanding of space transportation systems and their environmental impact.
You will be employed by the host organization for 36 months.
You will participate in international conferences and secondments to other organisations within the SLICE network and in outreach activities targeted at a wide audience.
A competitive salary according to MSCA regulations (see page 118ff, https://ec.europa.eu/info/funding-tenders/opportunities/docs/2021-2027/horizon/wp-call/2023-2024/wp-2-msca-actions_horizon-2023-2024_en.pdf ), including a living allowance, a mobility allowance and, if eligible, a family allowance. The stated allowances represent the gross funding amounts. Employer contributions to social security, health insurance, and other statutory costs will be deducted in accordance with the applicable national regulations.


Please find additional information in the Information package for Marie Curie fellows in doctoral networks (https://op.europa.eu/s/z831).