Lead, Structural Analysis Engineering (Stress, Fatigue & Damage Tolerance)

At Relativity Space were building rockets to serve todays needs and tomorrows breakthroughs. OurTerran R vehicle will deliver customer payloads to orbit meeting the growing demand for launchcapacity. But thats just the start. Achieving commercial success with Terran R will unlock newopportunities to advance science exploration and innovation pioneering progress that reaches beyondthe known.

Joining Relativity means becoming part of something where autonomy ownership and impact exist at every level. Here youre not just executing tasks; youre solving problems that havent been solved before helping develop a rocket a factory and a business from the ground up. Whether youre in propulsion manufacturing software avionics or a corporate function youll collaborate across teams shape decisions and see your work come to life in record time. Relativity is a place where creativity and technical rigor go hand in hand and your voice will help define the stories were writing together. Nowis a unique moment in time where its early enough to leave your mark on the product the process andthe culture but far enough along that Terran R is tangible and picking up momentum. The mostmeaningful work of your career is waiting. Join us.

About the Team:

The Integrated Performance team owns the holistic view of how Terran R comes together ensuring that every system on the vehicle and ground is capable of achieving ambitious performance reliability and reusability goals. The team works across the full launch systemfrom trajectory design and aerodynamics to reliability analysis and post-flight data reviewwith technical leadership influence across the entire product lifecycle. Beyond analysis team members engage hands-on with hardware testing and operations with the authority to lead and drive meaningful programmatic change.

The Integrated Analysis group accelerates Relativitys hardware engineering through advanced analysis life prediction and modern tools. The team enables robust lightweight and reusable structures by leading the integration of fatigue fracture durability and inspection considerations early in design and throughout vehicle maturation.

About the Role:

As a Structural Analysis Lead you will provide technical leadership for the structural integrity strength durability and life management of flight hardware across the vehicle. You will be responsible for defining and executing structural analysis strategies spanning static strength fatigue and damage tolerance fracture mechanics and structural dynamics.

In this role you will guide the development verification and certification of primary and secondary structures from early design through flight operations. You will work closely with design materials manufacturing and test teams to ensure structurally robust designs that meet performance reliability and reusability requirements.

Cross-Functional Leadership & Tools

• Oversee a team of analysts while maintaining direct technical contribution
• Provide technical mentorship and guidance to structural analysts and engineers
• Collaborate with design materials manufacturing and test teams to ensure structurally robust and manufacturable designs
• Establish and improve structural analysis standards best practices and verification workflows
• Develop automation and analysis tools using scripting environments such as Python or MATLAB to improve analysis efficiency

Structural Analysis Leadership

• Lead structural analysis activities for major vehicle structures across component subsystem and vehicle levels
• Define structural analysis methodologies requirements and design margins for flight-critical hardware
• Provide technical leadership across static stress fatigue fracture mechanics and durability assessments

Stress & Structural Analysis

• Perform and review static and dynamic stress analyses for metallic and additively manufactured structures
• Develop and maintain finite element models using tools such as Nastran and Abaqus with pre/post environments such as Femap
• Evaluate structural margins including yield ultimate strength buckling thermal stress and dynamic response
• Support structural sizing and optimization of primary load-bearing structures

Fatigue & Damage Tolerance

• Develop fatigue life and durability predictions using SN/EN methods and fracture mechanics approaches
• Perform crack initiation and crack growth analyses using tools such as NASGRO and AFGROW
• Establish fatigue allowables crack growth limits inspection intervals and life limits for flight hardware
• Translate time-domain or spectral load environments into fatigue-relevant stress histories and cumulative damage metrics

Loads Modeling & Environments

• Translate flight ground acoustic and thermal environments into structural loads and responses
• Integrate loads and environments into structural analysis and fatigue life predictions
• Support multidisciplinary analysis for vehicle-level structural performance

Test Correlation & Structural Validation

• Lead correlation of structural and fatigue analyses with qualification and durability testing
• Support structural testing including component subsystem and full-scale structural tests. Investigate anomalies and structural failures and update analysis models accordingly
• Support structural life reassessment using test and flight data

About You:

• Bachelors degree in Mechanical Engineering Aerospace Engineering or a related discipline
• Experience leading or mentoring a team (either formally or informally)
• 5 years of experience in structural analysis fatigue & damage tolerance or structural life assessment
• Strong understanding of:
  • Static stress analysis
  • Structural mechanics
  • Fatigue and Fracture mechanics
  • Structural failure modes in aerospace hardware
• Proficiency with commercial finite element analysis tools such as:
  • Nastran
  • Abaqus
• Experience using pre/post-processing environments such as Femap
• Proficiency with fracture mechanics software such as:
  • NASGRO
  • AFGROW
• Experience converting time-domain or spectral loads into fatigue damage and life predictions
• Proficiency with engineering scripting or analysis languages such as Python or MATLAB
• Ability to independently scope execute review and defend structural analyses

Nice to Haves but Not Required:

• Masters or PhD in Mechanical or Aerospace Engineering
• Experience with launch vehicles reusable aerospace systems or flight-critical hardware
• Experience with additive manufacturing structural analysis and fatigue characterization
• Familiarity with Elastic-Plastic Fracture Mechanics (EPFM)
• Experience correlating structural fatigue or fracture predictions with test or flight data
• Prior experience defining structural design allowables or durability standards for aerospace systems

We are an equal opportunity employer and value diversity at our company. We do not discriminate on the basis of race religion color national origin gender sexual orientation age marital status veteran status or disability status.

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