Mechanical Architect

Infinite Orbits

Toulouse, France

About the Role

As the Satellite Mechanical Architect, you will own the mechanical design and integration strategy for our GEO satellite platform. This senior-level role requires deep technical expertise, creative problem-solving, and a hands-on approach. You’ll work across disciplines to architect mechanical systems that are robust, efficient, and tailored for the unique challenges of an in-orbit servicing mission.

Job Description

  • Lead the design and development of the satellite’s mechanical architecture, including structures, deployables, and thermal interfaces.
  • Perform or oversee FEA modelling and analysis for structural, thermal and thermoelastic to ensure compliance with mission and launch requirements.
  • Collaborate with cross functional teams, including avionics, propulsion, and systems engineering teams to ensure seamless integration to ensure seamless integration.
  • Manage mechanical integration and test activities from component-level through full spacecraft assembly.
  • Manage suppliers/partners involved in design, simulation, fabrication and testing.
  • Support environmental qualification testing (vibe, TVAC, shock), including test planning and data review.
  • Participate in design reviews and risk assessments throughout the development cycle.
  • Manage and provide mentorship to junior engineers and foster technical excellence across the team.
  • Responsible for maintaining documentation, including design specifications, test plans, performance reports. and ICDs.
  • Stay current with the latest advancements in propulsion technologies and space mission requirements, and apply this knowledge to ongoing and future projects.

Requirements

  • Bachelor’s degree in Mechanical or Aerospace Engineering (or related field).
  • Minimum 7 years of experience in satellite mechanical and thermal design.
  • Experience designing and integrating mechanical systems for large satellite platforms.
  • Proficiency with CAD and FEA tools (e.g., NX, CATIA, SolidWorks, ANSYS, NASTRAN).
  • Deep understanding of launch vehicle requirements, space environment effects, and mass/cg management.
  • Demonstrated experience in thermal-mechanical interface management and structural-thermal trade-offs.
  • Ability to prioritize tasks and adapt to changing project requirements in a dynamic environment.
  • Strong communication and interpersonal skills, with the ability to collaborate effectively with diverse teams.

Desirable Experience and Skills:

  • Experience with full satellite lifecycle - from conceptual design to launch and commissioning.
  • Familiarity with ECSS, NASA, or MIL-STD environmental qualification standards.
  • Experience with large deployables, antenna structures, or propulsion system integration.
  • Exposure to small-batch fabrication, rapid prototyping, or non-traditional manufacturing.
  • Hands-on AIT (Assembly, Integration & Test) experience, including GSE and cleanroom protocols.
  • Knowledge of radiation effects, outgassing, and thermal control strategies for GEO missions.
  • Experience interfacing directly with launch providers and mission assurance teams.

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