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Spacecraft Solar Array Engineer

Job in Ashburn, Loudoun County, Virginia, 20147, USA
Listing for: Overview Energy
Full Time position
Listed on 2026-07-01
Job specializations:
  • Engineering
    Electrical Engineering, Aerospace / Aviation / Avionics, Mechanical Engineer
  • Energy/Power Generation
    Electrical Engineering, Aerospace / Aviation / Avionics
Job Description & How to Apply Below

Spacecraft Solar Array Engineer

Overview Energy is a mission-driven team committed to delivering Space Solar Energy to the world. We operate at the intersection of space infrastructure and energy abundance, providing baseload power across entire continents 24/7, without seasonality or the need for batteries. Headquartered in the Washington, DC area and backed by world-class investors, we are advancing the next generation of clean energy technology.

The Role

Overview Energy's Spacecraft Solar Array Engineer leads the design, development, qualification, and in-orbit performance optimization of spacecraft solar array and power generation systems from concept through end-of-life. The role blends spacecraft power subsystem engineering, structural and thermal design awareness, and hands-on test and integration work to deliver reliable, lightweight, and highly efficient photovoltaic power solutions for orbital and deep-space missions. The ideal candidate has experience with space-rated photovoltaic technologies, deployable solar array mechanisms, and spacecraft power architectures, and can own the solar array subsystem from requirements definition through flight support.

Key Responsibilities

  • Architect and design spacecraft solar array systems, including cell technology selection, string and panel configuration, array sizing, and interfaces
  • Perform power budget development, orbital energy balance analyses, and end-of-life power predictions across mission scenarios, eclipse seasons, and pointing constraints
  • Develop detailed design specifications, interface control documents (ICDs), and technical documentation for solar panels, harnessing, deployment mechanisms, and array drive assemblies using CAD and industry-standard analysis tools
  • Conduct electrical, mechanical, and thermal analyses of solar array assemblies, including structural margins for launch loads, thermal gradients, degradation, and pointing performance impacts
  • Support design of deployment and articulation solutions (hinges, hold-down and release mechanisms, solar array drive mechanisms), working with mechanisms and structures engineers to balance stiffness, strength, mass, and deployment reliability
  • Define, plan, and execute qualification and acceptance test campaigns for solar array assemblies and subcomponents, including electrical, mechanical, environmental, and life testing
  • Work with manufacturing and supply chain to ensure design-for-manufacturability, process control, and traceability of space-qualified photovoltaic materials and components

Required Qualifications & Experience

  • Bachelor's degree in Electrical Engineering, Aerospace Engineering, Mechanical Engineering, or related field with a focus on power or space systems
  • 5+ years of experience in spacecraft power systems, spacecraft solar arrays, or closely related photovoltaic hardware for space applications (cell, module, panel, or array-level)
  • Strong proficiency with CAD and analysis tools for mechanical and/or electromechanical design, plus experience with solar array sizing and performance modeling
  • Experience with power system design (voltage regulation, string configuration, bypass diodes)
  • Experience with rapid prototyping and hands-on electrical and mechanical assembly
  • Experience in soldering techniques relevant to solar module assembly, including hand soldering, reflow methods, and cell interconnection (tabbing/stringing)
  • Experience with environmental and qualification testing relevant to flight hardware (e.g., vibration, shock, thermal vacuum, radiation), including test planning and data review
  • U.S. citizenship required

Preferred Skills & Experience

  • Graduate degree (M.S. or Ph.D.) in Electrical, Aerospace, or Mechanical Engineering with emphasis on spacecraft power systems or space photovoltaics
  • Hands-on experience with design and qualification of spacecraft solar arrays, solar array drive mechanisms, or power distribution hardware for flight programs
  • Experience with lightweight, flexible solar array stackups and associated support structures
  • Familiarity with space qualification and reliability standards (e.g., NASA, ECSS, MIL standards) applicable to power and structural hardware
  • Experience…
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