Lead architecture definition for avionics hardware platforms including compute modules, I/O boards, and communication interfaces.
Collaborate with systems, software, and mechanical teams to define system-level architecture and design trade-offs.
Define high-level hardware specifications and system interfaces (ICDs, power, thermal, signal).
Ensure architecture compliance with DO-254, MIL-STD, and other aerospace standards.
Guide schematic and layout design to align with platform requirements and constraints.
Conduct design reviews, risk assessments, and FMEA for architectural integrity.
Support system integration, debug, and hardware bring-up with verification teams.
Interface with customers and OEMs for requirement clarification, solution alignment, and design sign-offs.
Required Qualifications:
Bachelor's or Master's degree in Electrical Engineering, Electronics, or related field.
10+ years of experience in avionics hardware development, with at least 3+ years in an architecture/leadership role.
Strong understanding of digital and analog design, signal integrity, and power systems.
Expertise in avionics communication protocols (e.g., ARINC 429, MIL-STD-1553, Ethernet).
Experience with system-level modeling tools (e.g., SysML, MATLAB/Simulink).
Working knowledge of DO-254, DO-160, EMI/EMC considerations, and environmental testing.
Strong documentation, analytical, and leadership skills.
Preferred Qualifications:
Familiarity with hardware/software co-design principles and system simulation.
Exposure to obsolescence management, thermal management strategies, and high-reliability designs.
Previous collaboration with OEM/Tier-1 customers on aerospace programs.
Department: Transportation (India) Associate Skills Required: DO-254, system architecture, matlab, architecture, Sysml Years Of Exp: Above 10 Years Designation: Associate
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