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The role involves designing and testing fluid systems for New Glenn rocket, including managing specifications and vendor relationships, project management, and thermodynamic modeling using software tools.

Design and analyze cryogenic fluid systems for lunar landers, ensuring reliability in extreme environments. Lead requirements, design reviews, and procure components for lunar missions.

The engineer will design cryogenic propulsion systems components, focusing on CAD modeling, manufacturability, and structural analysis while mentoring junior engineers.

The Sr. Optical Amplifier Engineer will lead high-power fiber laser amplifier development, focusing on design, execution, and team collaboration for aerospace applications.

The Embedded Software Engineer II will develop and test flight software for the Blue Ring spacecraft, ensuring functionality and performance through collaboration and rigorous testing.

Execute acceptance, functional, and performance tests for recurring-production motion control hardware. Stand up and modify test fixtures, configure instrumentation and DAQ, run environmental tests (vibration, shock, thermal, TVAC), perform data acquisition and first-level analysis, document results, support anomaly investigations, and collaborate with design, quality, and technicians to maintain test readiness and calibration.

The Senior Electrical Engineering Lead will manage the avionics design and development for the Zero Boil Off cryocooler system, ensuring compliance with technical, cost, and schedule standards while leading a team of engineers.

The Technical Project Manager III will manage RF component development projects for lunar vehicles, ensuring technical compliance, budget adherence, and communication with stakeholders. Responsibilities include project oversight, establishing technical roadmaps, and collaborating with teams to meet program milestones.

The ECLS Hardware Engineer will design and develop hardware for Environmental Control and Life Support systems in spacecraft, including fluid systems and mechanical design. Responsibilities include managing the lifecycle of ECLS components and ensuring compliance with technical standards.

Lead architecture, design, and implementation of scalable flight software for a large satellite constellation. Define frameworks, core services (C&DH, telemetry, health monitoring, fault management), coding standards, secure OTA updates, and verification practices. Integrate with cross-disciplinary teams, support SIL/HIL testing, CI/CD and automated verification, and ensure cybersecurity and maintainability across the full flight software lifecycle.