Mission
As a Structures Analysis Engineer at PLD Space, your mission is to optimize and validate the [JR1] design solution, contributing to weight optimization and guaranteeing rocket’s performance. You will also be involved you in hardware testing which is a key aspect of the job since it will allow you to validate designs and FEM via test correlations.
Responsibilities
- Achieve stress justification for new designs by using hand calcs and FEA methods for composites and metals.
- Perform test predictions and test correlations in order to improve FEA confidence.
- Perform complex modelling by creating global finite element model (GFEM) and detailed models (DFEM) both primary and secondary structures.
- Perform linear and non-linear structural analyses.
- Perform linear buckling analyses.
- Perform random, sine and modal dynamic analyses.
- Participate in the review process, preparing the necessary reports, memos and formal compliance documents (written in English).
- Liaise with other functions when required to ensure stress requirements are needed.
Required Competencies
- Bachelor’s or Master’s degree in Aeronautical, Mechanical or related engineering.
- Experience with structural analysis, all methods are valuables (hand calculations, FEA linear, non-linear, buckling, explicit dynamics).
- Fundamental knowledge of metallic structure behaviour and failure modes like strength and stability.
- Experience with Finite Element Analysis software.
- Self-motivated and able to work under pressure to meet deadlines, dealing with situations that are constrained by time and managing different tasks at once.
- Proactive and good team worker.
- Knowledge in scripting software such as MATLAB, Python or VBA
- Fluent Spanish and English.
Valued Competencies
- Proficient in using Finite Element Analysis principles and associated tools. Experience with HyperWorks/HyperMesh and OptiStruct is desirable.
- Good Knowledge on MatLab and VBA Excel is desirable.
- In-depth knowledge of engineering principles and design techniques relation to composite materials, classical laminate theory and finite element modelling techniques.
- Knowledge in fatigue analysis.
- Understanding of spacecraft manufacturing methods and processes.
- Experience in FEA correlations, structures qualification or collaboration with testing
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