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Pillar Space

Reusable orbital infrastructure for payload hosting

Founding Lead Avionics Engineer

AvionicsConfirmed live in the last 24 hours
Full-timeLos Angeles, CA, USAHybrid

About the Job

Requirements

  • A bachelor's degree in Electrical Engineering, Computer Engineering, Aerospace Engineering, Physics, or a related technical discipline.
  • At least 8 years designing, building, testing, or flight-qualifying avionics or electronics for spacecraft, launch vehicles, aircraft, robotics, or other high-reliability systems.
  • Prior experience leading technical workstreams, managing engineers, mentoring junior and mid-level engineers, or building high-performing engineering teams.
  • Demonstrated ability to own complex hardware systems from early architecture through design, fabrication, test, qualification, and operational readiness.
  • Strong fundamentals in analog and digital circuit design, power electronics, embedded processors, and signal integrity.
  • Expert proficiency with schematic capture and PCB design tools such as Altium, Cadence, or KiCad, and a track record of taking boards from schematic through layout, fabrication, assembly, and bring-up.
  • Experience designing hardware that interfaces with real sensors, actuators, and processors, including power supplies, motor and valve drivers, data buses, and mixed-signal front ends.
  • Ability to read and write low-level firmware or test scripts such as C or Python, and partner with software engineers through board bring-up and debugging.
  • Experience with fault-tolerant hardware design, including redundancy, cross-strapping, fault containment, overcurrent protection, and safe power-up and power-down behavior.
  • Experience taking hardware beyond the bench into integration, environmental testing, hardware-in-the-loop, or representative testbeds.
  • Experience with disciplined hardware development practices, including design reviews, configuration management, component derating, and documented test procedures.
  • Lab fluency with oscilloscopes, logic analyzers, spectrum analyzers, power supplies, electronic loads, JTAG/SWD debuggers, EGSE, and test automation.
  • Ability to work independently with limited direction, identify the right next problem to solve, and drive technical work from ambiguity to qualified flight hardware.
  • Ability to make practical system-level tradeoffs across performance, schedule, cost, mass, power, reliability, testability, and mission risk.
  • Ability to lead through influence in a cross-functional environment spanning flight software, GNC, propulsion, thermal, mechanical, systems, and mission operations.
  • Applicants must be a U.S. citizen or national, lawful permanent resident, refugee, asylee, or eligible to obtain the required authorizations from the U.S. Department of State.

Responsibilities

  • Own the avionics architecture from early design through development, integration, test, qualification, and flight operations.
  • Lead design of flight electronics, including flight computers, data handling units, power conditioning and distribution units, sensor and actuator interface boards, and motor, valve, and heater drivers.
  • Define power distribution and protection, including solar array and battery interfaces, regulation, load switching, fault protection, grounding, and bonding.
  • Architect redundancy, cross-strapping, fault containment, and failure-tolerant designs appropriate for flight-grade autonomous systems.
  • Integrate GNC sensors and actuators, propulsion electronics, and payloads with well-defined electrical and data interfaces.
  • Define electrical interfaces and vehicle data buses, including SpaceWire, CAN, Ethernet, MIL-STD-1553, RS-422/485, SPI, I2C, and UART, and own interface control documents with every subsystem.
  • Own RF and communications hardware, including radio and antenna selection, link budgets, and spectrum coordination with the ground segment.
  • Make build-versus-buy trades across COTS, upscreened, and rad-hard parts and units, and manage vendors and subcontractors through delivery.
  • Lead schematic capture, PCB layout, and design reviews, including worst-case circuit analysis, parts stress derating, board-level thermal analysis, and signal and power integrity.
  • Design for the space environment, including total ionizing dose, single-event effects, latchup protection, EMI/EMC, outgassing, and thermal-vacuum performance.
  • Own harness design, including wiring diagrams, connector and pinout definition, routing, and fabrication and testing alongside mechanical and integration teams.
  • Build avionics test infrastructure, including bench test equipment, EGSE, flatsats, hardware-in-the-loop rigs, and automated functional and acceptance testing.
  • Plan and execute qualification and acceptance campaigns, including vibration, shock, thermal cycling, thermal vacuum, EMI/EMC, and radiation testing.
  • Partner with flight software on processor and FPGA/SoC selection, board bring-up, and debugging, driving root-cause resolution across hardware and software on the bench and during integrated test campaigns.
  • Provide technical leadership across avionics, power electronics, RF, harnessing, and electrical test efforts.
  • Help hire, manage, mentor, and develop avionics and electrical engineers as the team grows.
  • Establish hardware engineering processes, including design standards, design reviews, parts and materials control, configuration management, requirements traceability, and verification discipline appropriate for flight-grade hardware.
  • Help define avionics requirements, interfaces, power, mass, and data budgets, verification plans, and failure-handling approaches for the vehicle.
  • Work closely with flight software, GNC, propulsion, thermal, mechanical, systems, ground software, and mission operations to close interfaces, deliver flight units, and field an integrated flight system.
  • Work closely with the founders and early engineering team to shape the technical roadmap, engineering culture, hiring plan, and long-term avionics strategy.
  • Represent the avionics function in cross-disciplinary design reviews, customer conversations, investor diligence, vendor discussions, and mission planning as needed.

Desired Qualifications

  • Demonstrated flight heritage: avionics the candidate helped design or build that has flown and operated on orbit.
  • Experience leading avionics, electrical, power, RF, or hardware test teams.
  • Experience managing engineers in a startup, aerospace company, defense contractor, launch company, robotics company, or other high-reliability technical environment.
  • Experience designing flight computers or data handling units, including processor, memory, and FPGA/SoC selection such as Xilinx/AMD Zynq, Microchip PolarFire, or rad-hard microcontrollers.
  • Experience with spacecraft electrical power systems, including solar arrays, lithium-ion batteries, maximum power point tracking, and power distribution and protection.
  • Experience designing for radiation, including part selection and screening, TID and SEE analysis, latchup protection, and radiation test campaigns.
  • Experience with GNC sensors and actuators or propulsion electronics such as valve drivers, pressure transducers, and thruster controllers.
  • Experience with RF and communications hardware, including S-band, X-band, or optical links, link budgets, and antenna integration.
  • Experience with spacecraft data buses and protocols, including SpaceWire, MIL-STD-1553, CAN, or CCSDS.
  • Experience with FPGA development in HDL (VHDL/Verilog) and hardware/software co-design.
  • Experience with EMI/EMC design and testing, including MIL-STD-461 and grounding, bonding, and shielding strategies.
  • Experience with flight harness design and fabrication, connector selection, and wiring standards.
  • Experience designing internally developed test infrastructure, including flatsats, EGSE, HIL rigs, and automated acceptance test stations.
  • Experience with environmental qualification and acceptance testing, including vibration, shock, thermal vacuum, and thermal cycling.
  • Experience with workmanship and parts standards for space hardware, including IPC J-STD-001 Space Addendum, NASA-STD-8739, EEE-INST-002, and GSFC-STD-7000/GEVS.
  • Experience with reliability and mission assurance, including FMEA, fault trees, worst-case circuit analysis, parts stress analysis, and hazard analysis.
  • Experience supporting avionics from prototype through flight operations, anomaly response, and post-flight reconstruction.
  • Experience in early-stage startups, small high-performing teams, or environments where engineers must own broad technical scope.
  • Experience recruiting, interviewing, closing, and onboarding exceptional technical talent.

About the Company

Pillar Space

Reusable orbital infrastructure for payload hosting

Pillar Space builds reusable satellites that stay in orbit and act as rentable infrastructure for other payloads. A customer launches a payload in a standardized adapter, and Pillar Space’s satellite autonomously docks with it in low Earth orbit, then supplies power, data, thermal management, mobility and mission operations for the lease, with an optional capsule re-entry to return finished products to Earth. This on-orbit docking-based service lets customers test and operate in microgravity without owning their own spacecraft. The team includes veterans from Northrop Grumman’s Mission Extension Vehicles and alumni from SpaceX and Impulse Space, backed by South Park Commons, with a first mission window targeted for 2028 to provide persistent orbital infrastructure for biotech, semiconductors, materials, and defense clients.

Company size
1-10
Company stage
Not listed
Total funding
Not listed
Headquarters
Los Angeles, CA
Founded
2026

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