Space Propulsion System Performance Intern - Toulouse

Pangea Propulsion

Toulouse

On-site

EUR 12,000 - 19,000

Full time

5 days ago
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Job summary

Pangea Propulsion in Toulouse is seeking a motivated System Performance Intern to join our team. During a six-month internship, you will support system-level design, modelling and performance analysis for Kronos full-flow staged-combustion rocket engines.

You will work with engineers across combustion, fluidics, turbomachinery to connect engine requirements with cycle modelling and subsystem performance. The role requires a MSc in Aerospace Engineering or equivalent, solid fundamentals in

Qualifications

  • MSc in Aerospace Engineering or equivalent.
  • Experience with numerical modelling and analysis.
  • Strong fundamentals in thermodynamics, fluid mechanics and heat transfer.
  • Understanding of liquid rocket propulsion and rocket-engine cycles.
  • Ability to analyze coupled systems and interpret simulation results.
  • Basic programming in Python and/or MATLAB.

Responsibilities

  • Develop, modify and run system-level engine models in EcosimPro/ESPSS.
  • Analyse nominal operating points and engine envelopes.
  • Support engine-cycle optimisation and system design trade-offs.
  • Perform sensitivity studies on design and operating parameters.
  • Translate results into conclusions, maps and envelopes.
  • Maintain System Performance documentation for design reviews.
  • Collaborate with combustion, fluidics and turbomachinery to integrate evolving subsystem designs.

Skills

Numerical modelling
Python
MATLAB
Thermodynamics
Fluid mechanics
Heat transfer

Education

MSc in Aerospace Engineering

Tools

EcosimPro/ESPSS

Job description

Pangea Propulsion in Toulouse is seeking a motivated System Performance Intern to join our team. During a six-month internship, you will support system-level design, modelling and performance analysis for Kronos full-flow staged-combustion rocket engines.

You will work with engineers across combustion, fluidics, turbomachinery to connect engine requirements with cycle modelling and subsystem performance. The role requires a MSc in Aerospace Engineering or equivalent, solid fundamentals in

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