The Exploration Company

Thermo-mechanical Engineer

Bordeaux, FranceFull time€50,000 - €70,000 / yearPosted 13 days ago
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Here at The Exploration Company, we are developing, producing, and operating Nyx, a modular and reusable space orbital vehicle that can eventually be refuelled in orbit and that can carry cargo - and potentially humans in the longer run.

The heart of a spacecraft lies in its engines, and that's why we, at The Exploration Company, are dedicated to developing our own cutting-edge Propulsion Systems ensuring the highest level of efficiency and reliability in our space endeavours.

We are seeking a talented Thermo-mechanical Engineer to join our Future Project division. As a key member of our engineering team, you will be responsible for designing, analyzing, and optimizing combustion devices for cryogenic rocket engines, with a focus on the main thrust chamber assembly.

KEY RESPONSIBILITIES

- Support structural and thermal analysis of combustion device hardware including injector heads, faceplates, combustion chambers, manifolds, and structural interfaces.

- Perform finite element analysis (FEA) and establish practical design suggestions and establish design recommendations, and margin assessments for hardware development.

- Develop and apply analytical and reduced-order models to estimate heat transfer, structural loads, and thermal boundary conditions to inform design trades and hardware maturation.

- Support hardware development and maturation, including design iteration, development planning, test definition, and post-test assessment of structural and thermal performance.

- Drive life assessment activities, including low-cycle fatigue, thermal fatigue, cyclic loading, margin tracking, and damage accumulation for reusable hardware.

- Own structural reliability and lifecycle assessments of combustion hardware, including low-cycle fatigue, thermal fatigue, cyclic loading, and thermo-mechanical failure risk evaluation.

- Collaborate with combustion and fluid engineers to translate predicted heat flux distributions, pressure fields, and flow ch...