Propulsion CAD & Stress Analyst — Thrust Chamber (TCA)

Atlas Metrics; Bordeaux; Sur place; EUR 40 000 - 65 000; Plein temps

Résumé du poste

The Exploration Company in France is seeking a CAD & Stress Analyst to design and structurally justify propulsion hardware, with a focus on the thrust chamber assembly. You will own parts from initial CAD layout through to final stress justification, collaborating with manufacturing and test teams to bring flight hardware from concept to qualified design.

During design you will perform CAD design, hand calculations and FEA to substantiate margins of safety under mechanical, thermal and pressure

Qualifications

• Bachelor's degree in Aerospace or Mechanical Engineering.
• Over 1 year of CAD design and stress analysis experience.
• Strong CAD skills to take a part from concept to detailed design.
• Experience in structural/stress analysis including hand calculations and FEA.
• Familiarity with manufacturing processes; CFD is a plus.
• Excellent collaboration and English proficiency.

Responsabilités

• Design the thrust chamber & injector propulsion hardware in CAD from concept to detailed design.
• Perform stress analysis (hand calculations and FEA) to substantiate margins of safety.
• Select materials and define manufacturing processes with producibility in mind.
• Collaborate with propulsion, thermal and fluidic engineers to translate requirements into design.
• Establish interfaces, drawings and data, ensuring configuration control and traceability.
• Conduct trade studies and justify design decisions with analysis.
• Elaborate and maintain structural analysis reports for design reviews.
• Support test requirements to validate analytical models and assumptions.
• Produce and maintain documentation of design choices and trade-offs.

Connaissances

CAD design

Stress analysis

FEA

English fluency

Formation

Bachelor's degree in Aerospace or Mechanical Engineering

Outils

ANSYS

Abaqus

Description du poste

The Exploration Company in France is seeking a CAD & Stress Analyst to design and structurally justify propulsion hardware, with a focus on the thrust chamber assembly. You will own parts from initial CAD layout through to final stress justification, collaborating with manufacturing and test teams to bring flight hardware from concept to qualified design.

During design you will perform CAD design, hand calculations and FEA to substantiate margins of safety under mechanical, thermal and pressure