We are seeking an experienced Stress Analyst to support the analysis and validation of ground systems, umbilical hardware, launch infrastructure, and transportation/handling tooling. The ideal candidate will have a strong background in structural analysis, finite element modeling (FEA), and aerospace or ground support equipment, with the ability to work closely with design teams to support engineering development and design validation efforts.

Location: Kent, WA
Job Type: Contract-to-Hire (REMOTE)
Pay Rate: $65 - $80 per hour (DOE)
Schedule: Full-Time | Monday-Friday (Overtime as needed)

• Perform structural and dynamic analyses to validate umbilical systems during launch and abort operations.
• Evaluate disconnect timing, clearance requirements, and load conditions.
• Analyze launch pad structures, support equipment, and integrated mechanical systems.
• Support development of load cases and design validation activities.

• Analyze test fixtures, stands, instrumentation hardware, and leak-check equipment.
• Perform structural analysis on lifting fixtures, transport frames, handling rings, and associated tooling.
• Evaluate load paths, rigging configurations, rated loads, and safety factors.

• Develop hand calculations and finite element analysis (FEA) models to support design validation.
• Prepare analysis reports for engineering releases and design reviews.
• Collaborate with design and drafting teams to support structural design decisions.
• Ensure compliance with applicable engineering standards and safety requirements.

• Bachelor's degree in Mechanical, Aerospace, Structural Engineering, or a related field.
• Experience performing structural analysis using hand calculations and FEA methods.
• Proficiency with ANSYS, Nastran, Abaqus, or similar analysis tools.
• Strong understanding of static, dynamic, thermal, and load path analysis.
• Familiarity with factors of safety, rated loads, and lifting/handling standards such as NASA-STD-8719 or ASME BTH-1.

• Experience with launch vehicle ground systems, umbilicals, or test equipment.
• Familiarity with NASA MSFC engineering standards and processes.
• Experience supporting launch, abort, transportation, or handling load case development.

INDH