PpJoin to apply for the bSenior Electrical Power Engineer /b role at bThales /b /p pA Joint Venture between Thales (67%) and Leonardo (33%), Thales Alenia Space is a global space manufacturer delivering, for more than 40 years, high‑tech solutions for telecommunications, navigation, Earth Observation, environmental management, exploration, science and orbital infrastructures. Thanks to our diversity of skills, talents and cultures, we have Space to Connect, Secure Defend, Observe Protect, Explore, Travel Navigate. /p pWe are looking for an Electrical Engineer with specific knowledge of electric motor drives and RFC analysis. /p h3Responsibilities /h3 ul liAssess and analyze mission System and Operational Requirement Documents, SRD / ORD. /li liInterface with main peers (System E2E, Avionics, Payloads). /li liImplement Electrical and EMC/RFC architectures. /li liAssess electrical interface resources, sizing and budgets. /li liAssess RFC issues through modeling and analysis. /li liImplement power architecture in simulation environments. /li liAssess energy balance, resources sizing and justification. /li liLead and conduct system-level and sub–system electrical EMC IVVQ. /li liSupport AIV across product life cycles. /li liSupport OPS team for SVTs, FOP, LEOP simulations, LEOP and commissioning. /li liLead assessment of motor drives interfaces and performances. /li liAssess mitigation techniques of the impinging electric field generated by satellite antennas and equipment using dedicated radar absorber materials and computational solvers (e.g. CST). /li liEMC and RFC satellite architecture definition, sizing and justification. /li liConduct circuit analyses. /li liESD (internal bulk charging, external surface charging, discharge) analyses. /li liMagneto static field analyses. /li liRFC and launch vehicle compatibility analyses. /li liEMC and RFC requirements specification. /li liEMC budgeting, frequency and control plan definition. /li liEMC corrective actions design (e.g. filtering, shielding, gasketing). /li liEMC design rules definition for harness. /li liEMC testing at equipment level (setup, requirements, validation). /li /ul h3About You /h3 pbEducation and experience /b /p ul liMaster’s Degree in Electrical/Electronic/Telecommunication Engineering or similar, with explicit focus on radio frequency and EMC. /li liFluent in English (C1 or above), both listening and reading. /li liAt least 2 years of experience in a similar position with a background in Earth Observation, Navigation, or Telecom platforms / spacecraft design and test phases up to launch/LEOP and commissioning. /li /ul pbSkills and knowledge /b /p ul liSystem requirements analysis, flow down and verification. /li liElectrical and power design and sizing. /li liDefinition and management of design documentation: specifications, performance analysis, interfaces, budgets, validation. /li liAnalysis, simulation and validation of supply systems and equipment for mission scenario fulfilment. /li liSupport satellite test campaigns during AIT, launch and in‑orbit phases for power simulation predictions. /li liAnalog electronics. /li liPower conditioning systems such as Shunt (S2R, S3R, S4R) and MPPT (Buck, Boost). /li liElectromagnetics, antennas and propagation topics. /li liRadio frequency system sizing. /li liRLC filters and circuit theory. /li liMATLAB/Simulink programming. /li liAnalysis tools (CST, FEKO, ADS, Keysight, ORCAD, SPIS). /li liRequirement analysis (IBM Rational Doors). /li liEMC engineering standards: MIL‑STD‑461, MIL‑STD‑462, MIL‑STD‑464, MIL‑STD‑1809, ECSS‑E‑ST‑20C, ECSS‑E‑ST‑20‑06C, ECSS‑E‑ST‑20‑07C, ECSS‑E‑HB‑20‑07, NASA‑HDBK‑4002, NASA‑TP2361. /li liPlasma interactions with RF (considered a plus). /li liMagnetic field interactions with electrical propulsion subsystem (considered a plus). /li /ul pbPersonal attributes /b /p ul liCustomer focused, proactive attitude. /li liOrganized and methodical approach with strong communication skills. /li liAbility to manage multiple tasks independently and within a team. /li liStrong results orientation within time and cost constraints. /li liProblem‑solving attitude. /li /ul pLocation: Rome (primary). Availability for short‐term travel to other locations and 24‑hour shifts may be required. /p pEmployment type: Full‑time. Permanent position. /p /p #J-18808-Ljbffr