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Antares Nuclear

Develops autonomous microreactors for remote power

Senior Structural Engineer - Space

Materials & StructuresConfirmed live in the last 24 hours
Full-timeTorrance, CA, USA$145k - $185k /yr

About the Job

Requirements

  • A bachelor's degree in Mechanical Engineering, Aerospace Engineering, Civil/Structural Engineering, Engineering Mechanics, or a related technical discipline is required.
  • At least 5 years of experience in structural analysis, stress analysis, structural dynamics, aerospace structures, spacecraft hardware, launch vehicle hardware, mechanical systems, or a related field is required.
  • Strong fundamentals in solid mechanics, strength of materials, structural dynamics, vibration, fatigue, bolted joints, load paths, stiffness, and stability are required.
  • Experience building and running finite element models for complex mechanical or aerospace hardware is required.
  • Experience analyzing static loads, modal response, random vibration, acoustic environments, fatigue, thermal stress, or coupled structural loads is required.
  • The ability to work long hours and weekends as necessary to support critical milestones is required.

Responsibilities

  • Own stress analysis and structural dynamics for space nuclear hardware, including component, assembly, subsystem, and integrated vehicle-level structures.
  • Support mechanical design and perform targeted structural design work for brackets, panels, reactor support structures, radiator structures, payload interfaces, test fixtures, and flight-like development hardware.
  • Perform first-order hand calculations and rapid analytical assessments for stress, stiffness, margin, load paths, bolted joints, welds, bonded joints, fasteners, interfaces, and structural stability.
  • Build, correlate, and maintain finite element models at the component, assembly, subsystem, and integrated system level.
  • Run detailed structural analyses, including static strength, stiffness, modal, random vibration, acoustic, coupled loads, thermal stress, coefficient of thermal expansion mismatch, fatigue, and shock-related assessments.
  • Support coupled thermal-structural analysis for space nuclear systems, including thermal stress, gradients, interface distortion, alignment effects, and thermomechanical compatibility between dissimilar materials.
  • Define structural analysis plans, load cases, boundary conditions, assumptions, margins, and verification approaches for flight and development hardware.
  • Develop plans for launch loads derivation, test loads definition, qualification strategy, acceptance testing, and structural verification.
  • Work with systems and vehicle teams to interpret launch provider environments, derive subsystem-level loads, and flow loads into design and test requirements.
  • Specify vibration, modal, acoustic, and structural development tests for components, assemblies, and subsystems.
  • Own vibration test planning and execution, including fixture design, instrumentation planning, test article preparation, test procedure development, data review, anomaly resolution, and post-test correlation.
  • Support procurement, commissioning, and operation of in-house vibration test capability, including vibration table requirements, facility integration, test safety, instrumentation, and operating procedures.
  • Participate in design reviews, test readiness reviews, failure reviews, and customer-facing technical reviews, clearly communicating structural risks, margins, model assumptions, and verification status.
  • Drive root-cause investigations for structural failures, test anomalies, model-test correlation gaps, and hardware nonconformances.
  • Develop reusable analysis methods, templates, and workflows that improve structural design speed, consistency, and technical rigor across Antares space nuclear programs.

Desired Qualifications

  • A master's degree or higher in Mechanical Engineering, Aerospace Engineering, Engineering Mechanics, Structural Dynamics, or a related field is preferred.
  • Experience with spacecraft, launch vehicles, satellites, payloads, space mechanisms, defense systems, nuclear systems, or other high-reliability aerospace hardware is preferred.
  • Experience with launch loads derivation, coupled loads analysis, notching, force limiting, sine vibration, random vibration, acoustic testing, shock testing, modal survey testing, or model correlation is preferred.
  • Experience planning, specifying, and executing vibration, modal, acoustic, or structural qualification or development tests is preferred.
  • Experience owning vibration test campaigns, including fixture design, accelerometer placement, control strategy, test procedure development, data interpretation, and post-test model correlation is preferred.
  • Experience selecting, procuring, commissioning, or operating vibration test equipment, including electrodynamic or hydraulic shakers, slip tables, amplifiers, controllers, fixtures, and instrumentation is preferred.
  • Experience with finite element analysis tools such as NASTRAN, FEMAP, Patran, Abaqus, ANSYS, HyperMesh, OptiStruct, Simcenter, NX, or equivalent structural analysis software is preferred.
  • Strong familiarity with Python and git-controlled code repositories is preferred.
  • Experience with coupled thermal-structural analysis, coefficient of thermal expansion mismatch, high-temperature structures, refractory materials, radiator structures, heat pipes, reactor support hardware, or nuclear-adjacent mechanical systems is preferred.
  • Experience with fatigue, fracture mechanics, creep, buckling, nonlinear contact, preload, bolted joint analysis, bonded joints, weldments, or composite structures is preferred.
  • Experience supporting structural thermal optical performance analysis or structural distortion analysis for precision payloads, optical systems, sensors, or thermally sensitive space hardware is preferred.
  • Familiarity with aerospace structural standards, launch provider environment definitions, NASA or Department of Defense test practices, or qualification and acceptance test philosophies is preferred.
  • Experience developing structural verification plans, analysis reports, test plans, test readiness review packages, and design review materials is preferred.
  • Strong practical judgment in early-stage development environments, including the ability to distinguish analysis depth necessary for risk reduction from analysis that slows hardware iteration, is preferred.

About the Company

Antares Nuclear

Develops autonomous microreactors for remote power

Preparing company description.

Company size
51-200
Company stage
Grant
Total funding
$765.1M
Headquarters
Los Angeles, CA
Founded
2023

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