Propulsion Engineer

About the Role

We are seeking a highly motivated Propulsion Engineer with hands-on experience in cryogenic propulsion systems and turbopump-fed rocket engines. The ideal candidate should possess strong expertise in the design, development, testing, and optimization of liquid propulsion systems, with a thorough understanding of Liquid Oxygen (LOX) handling, storage, and combustion characteristics.

Key Responsibilities

• Design, analyze, and develop cryogenic liquid propulsion systems for rocket engines.
• Develop and optimize combustion chambers, injectors, turbopumps, feed systems, and nozzles.
• Perform propulsion system sizing, thermodynamic cycle analysis, and engine performance calculations.
• Design and validate cryogenic propellant feed systems.
• Conduct combustion performance analysis, ignition sequence development, and engine startup/shutdown optimization.
• Support component-level and integrated engine testing, including hot-fire tests and performance evaluation.
• Perform thermal, structural, and fluid flow analyses to improve engine efficiency and reliability.
• Collaborate with multidisciplinary teams including structures, avionics, GNC, manufacturing, and systems engineering.
• Prepare technical documentation, design reports, and verification plans.
• Ensure compliance with safety standards for cryogenic propellant handling, storage, and testing.

Key Technical Competencies

• Cryogenic Propulsion Systems
• Liquid Rocket Engines
• Turbopump Design & Analysis
• Liquid Oxygen (LOX)
• Cryogenic Fluid Systems
• Combustion & Ignition Systems
• Propellant Feed Systems
• Engine Performance Analysis
• Thermal Management & Regenerative Cooling
• CFD & FEA Analysis
• Rocket Engine Testing & Validation