
Spacecraft Systems Engineer
- Torrejón de Ardoz, Madrid
- Permanente
- Tiempo completo
- EPS (Electrical Power Subsystem)
- Propulsion
- Onboard Data Handling (OBDH)
- AOCS (Attitude and Orbit Control System)
- Communication and TT&C systems
- Associated sensors and actuators
- Assess customer and mission needs to define system requirements, technical parameters, and ensure compatibility of all interfaces.
- System Architecture: Develop and maintain the spacecraft system architecture, ensuring consistency and alignment across all subsystems.
- Lead the design interdisciplinary coherence, development, and verification of:
- EPS: power generation, storage, distribution, and regulation.
- OBDH: operational modes, redundancy, FDIR, data buses, TM/TC.
- Propulsion: chemical and/or electric architectures, mission integration, and AOCS interfaces.
- AOCS: sensors, actuators, control algorithms, operational modes, and redundancies.
- Communication systems: telemetry, telecommand, and tracking links, including RF and SDR platforms.
- Perform trade-off analyses, simulations, and optimization of mass, power, cost, and performance at system level.
- Coordinate hardware and software integration across subsystems.
- Conduct environmental and functional validation testing at spacecraft level.
- Lead troubleshooting and anomaly resolution throughout the entire project lifecycle.
- Prepare and maintain technical documentation: requirements, ICDs, design reviews, and verification plans.
- Bachelor's or Master’s degree in Electrical Engineering or Aerospace Engineering or a related field.
- Master’s or PhD Electrical Engineering or Aerospace Engineering related technical discipline is a plus.
- At least 10 years working in spacecraft systems engineering or in key subsystems (EPS, OBDH, Propulsion, or AOCS).
- EPS: solar arrays, batteries, BMS, power distribution/regulation, EMC, fault tolerance.
- Propulsion systems: chemical/electric propulsion, mission integration.
- OBDH: FDIR, redundancies, buses, TM/TC, operational modes.
- AOCS: sensors, actuators, orbit and attitude control, algorithms.
- Communications: TT&C, RF, antennas, protocols (CAN, SpaceWire, Ethernet, RS-4XX).
- Experience with requirements management tools.
- Familiarity with reliability, FMECA, radiation and Worst Case analysis and tools.
- Knowledge of radiation-hardened electronics and space-qualified components.
- Hands-on experience with avionics hardware.
- Understanding communication protocols, such as CAN, RS-4XX, Ethernet, SpaceWire and others.
- Experience with digital, analog, mixed signal, and power design and analysis processes for space programs form a systems point of view.
- Hands-on experience with spacecraft integration and environmental testing (thermal vacuum, vibration, radiation and EMC/EMI).
- Familiarity with antenna and RF systems for spacecrafts TT&C.
- Experience working with product/component developers and vendors supply chain.