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Space Dynamics Laboratory

Nonprofit laboratory for space and defense research

Mid to Senior Spacecraft and Optical Payload Thermal Engineer

Aerospace EngineeringConfirmed live in the last 24 hours
Full-timeNorth Logan, UT, USA$102k - $160k /yrIn-person

About the Job

Requirements

  • A bachelor's degree in mechanical engineering, aerospace engineering, or a closely related technical field is required.
  • At least five years of relevant thermal engineering experience is required.
  • Demonstrated spacecraft, spaceflight payload, or closely comparable aerospace hardware thermal-design and analysis experience, including steady-state and transient modeling, is required.
  • Proficiency in Thermal Desktop, SINDA, FLUINT, or comparable spacecraft thermal-analysis tools, including independent model development, documentation, and interpretation, is required.
  • Experience supporting formal engineering design reviews such as PDR/CDR, with thermal requirements, margins, trades, and verification products, is required.
  • Experience planning, executing, analyzing, or correlating thermal-vacuum or thermal-balance tests of aerospace hardware is required.
  • Must be a U.S. citizen and able to obtain a U.S. Government security clearance.
  • Ability to collaborate across disciplines, communicate results clearly, defend engineering assumptions, and solve hardware-related thermal problems.

Responsibilities

  • Develop, analyze, integrate, and verify thermal-control solutions for NASA and Department of War small satellites and precision optical payloads, supporting concept and requirements development, thermal architecture trades, preliminary and critical design reviews, flight-hardware build and integration, thermal-vacuum testing, thermal-balance model correlation, payload calibration, and flight delivery.
  • Own or contribute to spacecraft and optical-payload thermal architectures, requirements, interface definitions, trade studies, and thermal-control hardware selection.
  • Develop, maintain, and document steady-state and transient thermal math models; evaluate orbital environments, operational cases, temperature limits, gradients, and design margins.
  • Prepare thermal analyses, verification matrices, design-review packages, and technical presentations for SRR, PDR, CDR, and test readiness reviews.
  • Work with mechanical, optical, electrical, systems, manufacturing, and integration teams to translate analysis into producible flight designs and resolve thermal interfaces.
  • Plan and support thermal-balance and TVAC tests, including test configurations, instrumentation, procedures, chamber operations, anomaly resolution, data reduction, and model correlation.
  • Support optical-payload TVAC calibration, thermal stability verification, as-built configuration evaluation, and flight acceptance and qualification activities.
  • Provide technical judgment on design margins, assumptions, risks, verification closure, and corrective actions; mentor less-experienced engineers as appropriate.
  • Depending on experience, serve as a thermal or mechanical project technical lead and support proposals.

Desired Qualifications

  • More than ten years of directly relevant experience.
  • Demonstrated end-to-end ownership of a spacecraft or payload thermal subsystem from concept through integration, environmental qualification, and flight delivery.
  • Experience with precision optical or infrared payloads, detector/focal-plane thermal management, thermal gradients, thermally induced alignment changes, and temperature stability.
  • Experience with optical-payload TVAC calibration, test-data reduction, thermal-model correlation, and test anomaly resolution.
  • Hands-on design and integration experience with MLI, radiators, thermal coatings, heat pipes, thermal straps, heaters, thermostats, sensors, and conductive interfaces.
  • Experience with cryocoolers, cryogenic instruments, or actively controlled optical assemblies.
  • Familiarity with NASA, Department of Defense, or ECSS spacecraft thermal verification and environmental test practices.
  • Experience using Python, MATLAB, or similar tools for thermal analysis automation and test-data processing.
  • Experience leading multidisciplinary technical efforts, mentoring engineers, and contributing to proposal estimates and thermal-design approaches.
  • A master's degree in mechanical engineering, aerospace engineering, or a related field.

About the Company

Space Dynamics Laboratory

Nonprofit laboratory for space and defense research

Space Dynamics Laboratory develops satellites, sensors and mission software for national defense, space exploration and scientific research. The nonprofit research corporation is wholly owned by Utah State University and operates as a university affiliated research center sponsored by the US Space Force. Its teams design and build instruments and spacecraft, test them for flight and develop ground systems that process mission data. Work spans government research partnerships and engineering programs, with support from initial mission concepts through deployment. The laboratory's operating roots date to 1959, and it took its present form through a 1982 merger; its headquarters are in North Logan, Utah.

Company size
1,001-5,000
Company stage
Not listed
Total funding
Not listed
Headquarters
North Logan, UT
Founded
1959

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