Spacecraft GNC Integration & Test Engineer Verified today

About the role

Quantum Space is redefining mobility and maneuverability in space with high-mobility spacecraft platforms supporting national security, civil, and commercial missions. We build fast and iterate quickly.

You will lead integration, verification, validation, and hardware testing of the Guidance, Navigation & Control subsystem. You own GNC hardware integration, anomaly resolution, and subsystem verification from component integration through flight acceptance. This is a hands-on role where simulation meets flight hardware.

What you will do

• Own integration, verification, validation, and flight acceptance of the spacecraft Guidance, Navigation & Control (GNC) subsystem from engineering development through spacecraft delivery.
• Develop, document, execute, and automate GNC verification procedures supporting subsystem, system, qualification, acceptance, and environmental testing.
• Plan and execute GNC hardware characterization and calibration activities, including inertial sensor characterization (Allan variance, bias instability, and angular random walk), sensor alignment, timing synchronization and phasing, and spacecraft magnetic characterization campaigns.
• Develop and operate Hardware-in-the-Loop (HITL), Software-in-the-Loop (SIL), FlatSat, and closed-loop simulation environments to verify flight software and spacecraft behavior.
• Integrate and validate spacecraft sensors, actuators, avionics, propulsion, and flight software while troubleshooting hardware, software, and system-level anomalies.
• Correlate high-fidelity simulation results with hardware test data to validate GNC algorithms, dynamic models, estimation performance, and control system behavior.
• Perform Monte Carlo analyses and mission-level performance assessments to verify spacecraft operating modes, robustness, and requirements compliance across expected uncertainties and disturbances.
• Analyze spacecraft telemetry and test data to identify root cause, recommend corrective actions, and improve GNC subsystem performance throughout integration, environmental test, and flight operations.
• Develop verification evidence supporting requirements closure and participate in technical reviews.
• Collaborate closely with systems, flight software, avionics, propulsion, mission design, and mission operations teams to deliver a fully verified and flight-ready spacecraft.

What you bring

• B.S. or M.S. in Aerospace Engineering, Mechanical Engineering, Electrical Engineering, Robotics, or related field.
• 3-8+ years of experience in spacecraft or high-reliability GNC development.
• Strong foundation in rigid-body dynamics, and classical/modern control theory.
• Experience with sensor fusion for spacecraft-relevant sensors (IMUs, star trackers, sun sensors, GNSS, ranging sensors).
• Experience developing, documenting, executing, and following formal test procedures and verification plans.
• Hands-on experience testing attitude control system hardware and ability to troubleshoot issues encountered during integration and test activities.
• Strong analytical and problem-solving skills with the ability to interpret technical data and recommend corrective actions.
• Experience collaborating within multidisciplinary engineering teams, with strong verbal and written communication skills to effectively communicate technical issues and risks.
• Proficiency with engineering analysis and simulation tools such as C++, MATLAB/Simulink, Python.