- Torrance, California, United States
- 2+ years
Lead the design, analysis, and testing of solid rocket motor propulsion systems to meet performance, structural, and thermal requirements.
Responsibilities
- Design and develop rocket motor systems, including grain geometry, case structures, insulation, and nozzle assemblies.
- Lead the architecture and detailed design of propulsion hardware to meet performance, structural, and thermal requirements.
- Perform internal ballistics, thermal, and structural analyses to ensure motor performance and reliability under extreme operating conditions.
- Advance the internal Castelion capabilities for analysis predictions and correlation to tests for solid rocket motor propellant and ignition systems.
- Work closely with structures, thermal, GNC, and manufacturing teams to ensure seamless integration of propulsion systems with the vehicle.
Requirements
- Bachelor's in Aerospace Engineering
- Master's in Aerospace Engineering
- PhD in Aerospace Engineering
- Nice to have: preliminary design
- Nice to have: conceptual design