Design and Analysis Integration Senior Manager

Analysis Integration

• Oversee design, development, test & evaluation, product verification/validation, and sustaining engineering
• Support troubleshooting of space‑flown hardware and conceptual design of propulsion LRUs and full propulsion systems

• Plan and oversee stress analyses (modal, quasi‑static, random vibration, fatigue, tubing) for components through full spacecraft
• Support multiple programs simultaneously across various lifecycle stages
• Interpret customer requirements, interface with customers, present analysis results, and prepare formal reports
• Coordinate resources for dynamic testing (random vibration, shock) of components and propulsion systems
• Oversee correlation of stress models to test data
• Manage direct reports responsible for flight hardware sign-off

• Bachelor’s degree or higher in Mechanical or Aerospace Engineering
• 10+ years of industry leadership experience (pay commensurate with experience)
• Extensive experience with CAD, Digital Twin tools, and NASTRAN/FEMAP
• Strong knowledge of spacecraft design, thermal, and structural analysis
• Strong written and verbal communication skills

• Full lifecycle spacecraft DDT&E experience, especially with electric propulsion
• Experience establishing/refining propulsion system design and analysis processes
• Experience with spacecraft design, thermal analysis, and stress/dynamic analysis
• Experience with dynamic testing (random vibration, shock, etc.)
• Experience with space or satellite hardware
• Work Environment & Physical Requirements
• Ability to work in office and manufacturing
• Able to meet program deadlines and occasional schedule flexibility