MAIN RESPONSIBILITIES
Key Responsibilities
Perform structural and thermal analysis (FEA) of rocket airframe, motor casing, and payload structures
Conduct CFD simulations of internal propulsion flowfields and external aerodynamics
Develop aero-thermal-structural coupled models
Analyze launch-induced environments (random vibration, acoustics, shock)
Support trajectory modeling and flight dynamics simulation
Correlate analytical models with test data and refine predictive tools
Collaborate with propulsion, structures, avionics, and systems engineering teams
Establish simulation standards, documentation practices, and verification methodologies
JOB REQUIREMENTS
Required Qualifications
Bachelor’s or master’s degree in Aerospace Engineering, Mechanical Engineering, or related field
Minimum 3–5 years of experience in computational simulation for aerospace systems
Strong background in FEA and/or CFD tools (e.g., ANSYS, Abaqus, NASTRAN, Fluent, OpenFOAM, or equivalent)
Experience with launch vehicle, missile, or high-speed aerospace systems preferred
Knowledge of dynamic loads, structural dynamics, and thermal environments
Proficiency in MATLAB, Python, or similar engineering computing tools
Strong analytical, problem-solving, and technical communication skills
Preferred Qualifications
Experience with sounding rockets, launch vehicles, or propulsion systems
Familiarity with systems engineering processes and model validation
Experience correlating simulation results with ground or flight test data
Leadership experience in technical teams
BENEFITS & WELFARE
Opportunity to contribute to a national-level aerospace development program
Collaborative, mission-driven engineering environment
Competitive compensation package
Flexible working arrangements
Long-term growth opportunities in advanced aerospace systems