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Here at The Exploration Company, we are developing, producing, and operating Nyx, a modular and reusable space orbital vehicle that can eventually be refuelled in orbit and that can carry cargo - and potentially humans in the longer run. Key Responsibilities: Design, develop, and maintain Electrical Ground Support Equipment (EGSE) sub-system and system level testing Define and implement EGSE hardware and software architectures tailored to specific test scenarios, AIT campaigns, and HiL environments Develop LabVIEW-based applications, for both desktop and real-time platforms (e.g., PXI, cRIO), supporting checkout, functional, and pre-launch test operations Integrate and configure NI VeriStand as part of real-time test setups, including simulation of spacecraft interfaces and umbilical/harness verification Design and support power, signal conditioning, and telemetry/telecommand interfaces between EGSE and the Unit/Spacecraft Under Test Support RF test activities for the TT&C chain, including uplink telecommand injection, downlink telemetry reception, and coordination of conducted/radiated test setups with the RF/comms subsystem team Collaborate with cross-functional teams (AIT, systems, RF, electrical, and FSW) to ensure seamless integration of EGSE hardware and software into functional test platforms Support test execution, data acquisition, logging, and automated reporting during integration, functional, and environmental test campaigns Create and maintain technical documentation, including EGSE architecture specifications, ICDs, code documentation, and user/operator guides Provide support for debugging, troubleshooting, and continuous improvement of EGSE and test platforms, including on-site support during AIT/launch campaigns Develop a robust and scalable EGSE software framework supporting reuse and modularity across projects Define test automation workflows Design and maintain EGSE-to-EUT interface hardware (harnesses, breakout boxes, simulators, load banks) with correct isolation, protection, and safety interlocks Own cable and harness design for EGSE-to-EUT connections, including pinout definition, connector selection, shielding/grounding strategy, and drawing generation Coordinate closely with electrical, RF, and systems engineers to ensure requirements traceability, interface compatibility, and test coverage Drive the continuous evolution of EGSE/HiL infrastructure, with an emphasis on performance, reliability, and maintainability Ensure all solutions meet space-grade quality, safety, and cleanliness standards (e.g., ESD, contamination control), aligned with project and range safety requirements Must-Have Skills and Qualifications Bachelor's or Master's degree in Electrical Engineering, Aerospace Engineering, Computer Science, or a related field Proficiency in LabVIEW, including desktop and real-time application development Hands-on experience with NI VeriStand in real-time test environments Familiarity with NI TestStand for test automation and execution management Solid understanding of EGSE/test platform architectures, hardware/software integration, and real-time systems Experience with spacecraft electrical interfaces: power distribution/simulation, discrete/analog telemetry, telecommand encoding, and standard space communication protocols (e.g., CAN, RS422/485, MIL-STD-1553, SpaceWire, Ethernet) Working knowledge of ICD development and requirements traceability between EGSE and flight hardware Ability to influence and shape ICDs and connector/pinout definitions upstream, rather than solely implementing to a fixed interface — working with electrical/systems engineers early in the design cycle to ensure EGSE testability and harness manufacturability Experience with cable/harness design, including connector selection, pinout/wiring diagrams, shielding and grounding practices, and generation of harness drawings (e.g., in ECAD tools or draw.io/Visio equivalents) Familiarity with RF test equipment and techniques (signal g

EGSE Engineer

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