Propulsion Aerothermal Analyst at Canada Rocket Company | CA | Rezi

Propulsion Aerothermal Analyst at Canada Rocket Company

Propulsion Aerothermal Analyst

Canada Rocket Company · CA

2 weeks ago

Propulsion Aerothermal Analyst

Canada Rocket Company · CA

16 days ago
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About the Role

We are seeking a Propulsion Aerothermal Analyst skilled in first-order calculations, CFD, and custom analysis code development. This role involves working across design, analysis, development, operation, and reuse scenarios in a dynamic environment. The position is ideal for a detail-oriented individual who wants to influence critical design decisions and shape the propulsion fluid systems for an orbital launch vehicle program.

Responsibilities

  • Perform aerothermal design of propulsion components, including injectors, thrust chambers, nozzles, valves, and other fluid system parts.
  • Analyze regenerative, film, and radiation cooling schemes and size cooling channels to maintain material temperature limits.
  • Analyze fluid transients, water hammer, priming, two-phase flow, cavitation, flow-induced loads, and feed system coupling across engine and stage fluid systems.
  • Perform thermal-fluid analysis of cryogenic propellant systems, covering tank thermal management, chill-down, boil-off, thermal conditioning, and insulation performance.
  • Develop and validate pressurization system models (autogenous, helium, or self-pressurizing) to determine pressurant requirements and predict ullage behavior.
  • Build, run, and maintain steady-state and transient thermal and fluid models using tools such as Thermal Desktop/SINDA, Fluent, CFX, EcosimPro, ESPSS, Flownex, or in-house Python/MATLAB codes.
  • Conduct trade studies and sensitivity analyses on system architecture, cooling, geometry, and operating points to guide design decisions.
  • Support cold flow, hot fire, stage test, and flight campaigns with pre-test predictions and post-test data reconciliation.
  • Identify thermal and fluid risks and failure modes, support anomaly investigations and root-cause analysis, and recommend design or operational mitigations.

Requirements

  • 5+ years of experience in one or more of the following: Aerothermal analysis of aerospace propulsion components, Creating and running 1-D flow networks for component sizing, Performing 3-D CFD analysis on propulsion components, Combustion analysis including liquid injection modelling, Aerothermal analysis of cryogenic propellant systems.
  • Demonstrated inclination toward a fast-paced, resource-constrained environment with rapid hardware development using iterative design-build-test cycles.
  • Bachelor's degree in mechanical engineering, aerospace engineering, or a related field.

Skills

  • CFD
  • Python
  • MATLAB
  • Thermal Desktop/SINDA
  • Fluent
  • CFX
  • EcosimPro
  • ESPSS
  • Flownex
  • Conjugate heat transfer analysis
  • CAD (NX)
  • Methane systems
  • Turbomachinery fluid analysis
  • Structural analysis

Experience Level

  • 5+ years

Education Level

  • Bachelor's degree in mechanical engineering, aerospace engineering, or a related field
  • Advanced degree in mechanical engineering, aerospace engineering, or a related field