Senior Analyst, Deployable Structures

E-Space

$140K — $210K *
Aerospace & Defense
Less than 5 years of experience
Job Overview by Ladders

Qualifications

  • BS, MS, or Ph.D. in Aerospace or Mechanical Engineering, or equivalent.
  • Proficiency in FEA structural analysis (Nastran, ANSYS) for dynamic and static problems.
  • Experience with structural analysis for flight or high-reliability hardware, focusing on margin calculations.
  • Expertise in structural dynamics, specifically modal analysis and eigenvalue methods.
  • Capacity to build and manage an integrated FEM from diverse team inputs.

Responsibilities

  • Own the integrated FEM of the antenna assembly, coordinating with subsystem teams.
  • Conduct deployed-state performance analysis: modal survey prediction and static deflection validation.
  • Develop and maintain structural requirements allocation from system-level to component-level.
  • Lead model-test correlation, updating model parameters based on test data.
  • Perform deployment analysis, aiding the Deployable Structures Test Engineer's predictions.
  • Evaluate structural risks from design changes and support anomaly investigations.
  • Establish and monitor the structural analysis error budget as designs evolve.

Benefits

  • Collaborative work environment with opportunities to influence aerospace innovation.
  • Direct engagement with hardware testing and integration activities.
  • Work within a focused team dedicated to advanced satellite technologies.
  • Potential for professional development in cutting-edge engineering practices.
Full Job Description
We are looking for a Senior Structures Analyst to own the structural analysis backbone of E-Space's Integrated Antenna Structure team. This person will develop and maintain the integrated finite element model of the deployed antenna assembly, perform structural performance and dynamics analysis, and establish requirements flow-down from system-level to component-level structural margins. This is a senior individual contributor role for someone with strong eigenvalue instincts, comfort with nonlinear and large-displacement problems, and opinions on what a deployable structure FEM is actually good for and where it breaks down. On-site in Texas preferred, California as alternate. Close proximity to hardware and test activities is important for this role. What you'll do: • Own the integrated FEM of the deployed assembly, incorporating structural element stiffness and mass properties from contributing subsystem teams and deployment mechanism boundary conditions. • Perform deployed-state structural performance analysis: modal survey prediction, static deflection under on-orbit loads (thermal, attitude control), and margin of safety verification. • Develop and maintain the structural requirements allocation, flowing from system-level performance requirements down to component-level stiffness, mass, and CTE requirements for each contributing team. • Lead model-test correlation at each level of the V&V test pyramid: update model parameters from test data, maintain a documented correlation record. • Perform deployment analysis (e.g., deployable element kinematics, tensioning loads, deployment force margins, system dynamics) in support of the Deployable Structures Test Engineer's test predictions. • Assess structural risk of design changes and interface deviations, and provide structural input to anomaly investigation teams. • Develop and maintain the structural analysis error budget, tracking margin consumption as design changes occur. Required Qualifications: • BS or MS or Ph.D. in Aerospace or Mechanical Engineering, or equivalent. • Proficiency in FEA structural analysis (Nastran, ANSYS, or equivalent) for modal, static, and linear dynamics problems. • Experience performing structural analysis for flight or high-reliability hardware, including margin of safety calculations and requirements compliance. • Experience with structural dynamics (modal analysis, frequency response, eigenvalue methods) not just static stress analysis. • Ability to build and maintain a system-level integrated FEM incorporating inputs from multiple contributing teams at different fidelity levels. Preferred Qualifications: • Ph.D. strongly preferred for the senior-level scope. • Experience with large deployable structures (antennas, solar arrays, booms, or lightweight flexible systems) including specific modeling challenges: geometric nonlinearity, low-stiffness modes, and large-displacement effects. • Experience with model-test correlation methodology, updating model parameters from test data and bounding residual correlation uncertainty. • Familiarity with deployment dynamics simulation tools (multi-body dynamics, flexible-body simulation). • Experience with structural error budgeting or requirements allocation across a multi-team program. • Python or MATLAB scripting for pre/post-processing of analysis data. $140,000 - $210,000 a year The estimated range is meant to reflect an anticipated salary range for the position in question, which is based on market data and other factors, all of which are subject to change. Individual pay is based on location, skills and expertise, depth of relevant experience, and other relevant factors. For questions about this, please speak to the recruiter if you decide to apply for the role and are selected for an interview. We are redefining how satellites are designed, manufactured and used-so we're looking for candidates with passion, deep knowledge and direct experience on LEO satellite component development, design and in-orbit activities. If that's your experience - then we'll be immediately wow-ed. E-Space is not currently able to provide employment sponsorship for candidates who do not hold work authorization for the location of this role.

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