Research and Design Engineering consulting for the Aerospace and Defense industry in the areas of Analog, Electromagnetic Compatibility and Radiation Effects.

Domain Leader for the Honeywell Aerospace Electromagnetic Compatibility Design group. Responsible for training and technical development of the engineers in the EMC design group of the Honeywell Aerospace Platform Electrical Design organization. Also responsible for development and maintenance of Best Practices for EMC and acting as delegate for the EMC Chief Engineer. Participated on the SAE AE-2 Lightning Committee, AE-4 Electromagnetic Compatibility Committee, CS-1 Space Environment Safety Committee and AIR6811 (DO-160/MIL-STD) Working Group.

Technical Manager for the Honeywell Aerospace Platform Electrical Design Electromagnetic Compatibility Design group. Managed EMC Design organization increasing group capabilities resulting in a first pass success rate of over 90 percent during EMI qualification testing.

Electronic Hardware COE process improvement efforts:• Led and drove the effort to update and rationalize the electronic hardware design processes across various functional groups within the Aerospace EHCOE. Updated processes to improve coordination and remove duplication of tasks.• Implemented conversion of the process documentation to an electronic web-based tool. Circuit designer for the Orion Crew Exploration Vehicle Solenoid Driver Output.• Responsible for the detailed electrical design of the Solenoid Output Driver PBA.Circuit design lead for the Kinetic Energy Interceptor Thrust Vector Controller.• Led the detailed electrical design team developing the Thrust Vector Controller.Circuit design lead for the TPE331 Digital Electronic Engine Control.• Responsible for leading a cross-site design team electrical engineers on the TPE331 Digital Electronic Engine Control program.Other relevant experience:• Led the electrical design and nuclear hardening efforts for the LV100 Engine Control and the J7 Digital Engine Control Unit for the AGT1500 engine used on the M1 Abrams Tank.• Performed the nuclear hardening and survivability design and analysis efforts for the Engine Thrust Control System, Auxiliary Power Controller and Oxygen Generation and Distribution System designs for the B-2 hardware designed at multiple Honeywell sites. Recognized by Northrop Grumman for excellence in performing the nuclear survivability analysis and hardening effort for the B-2 program.• Lead Circuit Designer for the replacement DV-2 Electronic Engine Controller for the L-59 aircraft.• Performed the radiation hardening design and analysis for electronic hardware designed at multiple Honeywell sites for the International Space Station. • Provided space radiation effects training to designers at the multiple Honeywell sites in support of the ISS design efforts.• Recognized for radiation hardening of the Integrated Motor Controller ASIC used on ISS hardware.

Instructor for courses covering AC and DC circuit theory, and mathematics applied to electronics.