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Combustion Engineer

Location: Pune, India (HQ) / On-site test facilities / Field testing locations as needed

Role Summary

As a Combustion Engineer, you will lead the design, development, and testing of advanced propulsion systems for high-performance aerospace and launch vehicle platforms. You’ll work closely with interdisciplinary teams to innovate and optimize combustion chamber configurations, injector designs, cooling mechanisms, and ignition systems for both atmospheric and vacuum environments.

Scope of Work

  • Design and analyze combustion chambers for liquid, solid, and hybrid propulsion systems.
  • Develop injector systems for cryogenic, hypergolic, and green propellants.
  • Simulate and validate combustion dynamics using CFD and thermal-fluid tools.
  • Collaborate on ignition systems, cooling designs (regenerative, ablative), and material selection for high-heat zones.
  • Support test campaigns, data acquisition, and performance validation at component and integrated levels.
  • Optimize engine performance under varying altitude and load conditions.

Nature of Work

This role demands a strong foundation in thermodynamics, fluid dynamics, and combustion theory. It is both hands-on and computational, involving prototyping, experimentation, and simulation. You’ll work in a fast-paced R&D environment where innovation, precision, and safety are paramount.

Key Responsibilities

  • Conduct design trade studies for engine cycle selection and chamber geometry.
  • Generate detailed thermal and flow simulations using tools like ANSYS Fluent, CONVERGE CFD, or OpenFOAM.
  • Coordinate with manufacturing teams for additive, cast, or machined parts.
  • Prepare technical documentation, safety reports, and validation checklists.
  • Work with test facility engineers during hot-fire tests and analyze thrust, ISP, and combustion efficiency data.

Eligibility & Requirements

  • Bachelor’s or Master’s degree in Aerospace, Mechanical, or Propulsion Engineering.
  • 2–6 years of experience in combustion system design or rocket engine development.
  • Proficiency in simulation tools (e.g., ANSYS, MATLAB, NASA CEA, or Cantera).
  • Knowledge of materials for high-temperature applications and thermal stress modeling.
  • Experience with hot-fire test procedures and data analysis preferred.
  • Strong analytical and problem-solving skills with clear documentation and communication ability.