Work Locations:

• Renton, WA
• Denver, CO
• Phoenix, AZ

Duration: 6-month contract, potential for extension or conversion

Hours: M-F 8-5, Hybrid Schedule

Responsibilities:

• Develop an embedded controller design that interacts with avionics systems (including sensors and electromechanical/electrohydraulic actuators).
• Own this design, and the rugged electronic hardware assemblies across the entire product life cycle, from concept and requirements definition, design, analysis, prototyping, schematic capture, layout, design review, test/verification (power-on, functional / acceptance / qualification testing) and through release to production.
• Support avionics controller architecture trade studies, analyses, performance characterization and specification, device selection, and controller roadmap direction.
• Support controller risk analyses, failure modes effects and criticality analyses (FMECA), design for test/manufacture/cost (DFx), and root-cause analysis of test discrepancies.
• Participate in program level technology development, mission assurance and safety initiatives, and avionics development process improvements.
• Effectively communicate development status, risks, and challenges to management.

Qualifications:

• Bachelor of Science in Electrical or Computer Engineering, or related disciplines
• A breadth of understanding in electronics hardware development such as developing complex circuit cards, consumer electronics, wireless devices, or other advanced electronic commercial or aerospace products
• Experience with analog, digital or mixed-signal circuit design, including analysis, simulation, test, troubleshooting, and part selection
• Knowledge of signal integrity, power, grounding, and general board layout principles
• Familiar with many of the following parts and their usage: microcontrollers, processors, FPGAs, ADCs, DACs, OpAmps, power supplies (linear, LDO, DC/DC), volatile memory (DDR), non-volatile memory (NAND, NOR, etc.), and MOSFETs
• Knowledge of common communication methods, such as RS232, RS422, I2C, SPI, LVDS, Ethernet, CAN, or PCIe
• Knowledge of radiation effects on electronics and how to apply this to designs targeting space applications
• Desire to work hands-on, both independently and as part of a team, throughout the development and production phases of the electronic assembly product lifecycle
• Ability to earn trust, maintain positive and professional relationships, and supply to a culture of collaboration

Desired:

• Master of Science in Electrical or Computer Engineering, or related disciplines
• Successful Candidates typically have 7 years of experience (5 years with Masters) in design, development, test, and operation of vehicle Avionics systems
• Experience with launch vehicle Avionics systems hardware development, integration, and test
• Basic or better knowledge of motor controller design and operation
• Demonstrated experience designing high reliability safety-critical, Class 2/3 board assemblies; familiarity with IPC-A-600/610, DO-254 and similar standards
• Scripting, Programming and Analysis: TCL, Python, Linux shell and Windows batch scripting; C / C ; MATLAB / Simulink, HSPICE and HFSS (or similar modeling/analysis tools)