As the Specialist Engineer responsible for avionics and data systems within the propulsion test team, I have played a pivotal role in the development of critical data acquisition software for the hybrid rocket motor test stand, enhancing its monitoring and control capabilities. Led the design and implementation of a comprehensive verification and validation testbenches for propulsion components. My proactive approach extended to defining and executing automated tests, ensuring propulsion avionics components were verified and validated to the design requirements.In a significant accomplishment, I collaborated closely with design engineers to provide valuable insights for design iterations and test stand reconfiguration based on test requirements. This collaborative effort contributed to the qualification and acceptance tests, facilitating the smooth integration of propulsion avionics components into the flight vehicle.Notably, as a key member of the propulsion test team, I was intimately involved with execution of 32 hybrid rocket motor hot fire tests on the test stand in Mojave since 2015. The pinnacle of this achievement was the testing of the most powerful hybrid motor used in a manned spaceflight, which was awarded the distinction of a Guinness World Record. This accomplishment underscores my commitment to excellence and innovation in propulsion development and testing, solidifying my position as subject matter expert in the field.

Consistently demonstrated expertise in advancing propulsion avionics and data acquisition systems. Spearheaded the development and redesign of data acquisition software and electrical architecture of hybrid rocket motor test stand , significantly enhancing the monitoring and control capabilities. With a focus on innovation, designed and implemented a comprehensive verification and validation testbench based on Components-Off-The-Shelf (COTS) testing hardware on propulsion avionics systems. Defined and executed automated tests to meticulously ensure that propulsion avionics components met stringent design requirements. Operating seamlessly within collaborative environments, provided invaluable insights to avionics hardware engineers for design iterations. Additionally, played a key role in qualification and acceptance tests, contributing significantly to the seamless integration of propulsion avionics systems into the flight vehicle. As an integral member of the propulsion test team, was responsibility for propulsion avionics and data acquisition systems during hot fire testing, ensuring precision and reliability of data.

Designed and developed software systems used to command and monitor a high fidelity testbed for multiple rocket engine configurations. Identified and implemented hardware configuration for integrating various sensors and actuators on the rocket test stand. Maintained and upgraded the PXI/Labview/Veristand systems that control the liquid rocket on the test stand. Assisted in the defining and executing automated tests to verify and validate rocket engine avionics design. Provided on-console support during critical test activities. Worked closely with other hardware and software design engineers in various phases of avionics development including requirements definition, design, board bring up, qualification and production. Contributed towards qualification and acceptance tests for flight computing hardware.

Initiated plans for development and implementation of powertrain control systems for testing.Developed, implemented, and evaluated model-based control and diagnostic algorithms designs for next-gen engine control systems. Specified, integrated, and performed troubleshooting of sensors and actuators commonly used for engine testing. Designed, developed and tested implementation of FPGA based combustion engine setpoint controller for testing single/multi cylinder engine configurations. Evaluated vehicle-based control systems and technologies. Integrated in-vehicle control system with analysis, simulations and control rapid-prototyping. Wrote software code and debugged vehicle-based embedded systems. Maintained and updated hardware-in-the-loop (HIL) systems for automotive validation testing. Designed interfaces between HIL tester and electronic modules to enable testing. Created software models to simulate hardware in HIL system. Collaborated with multi-disciplined engineering teams to understand functional requirements and implement appropriate solutions.

Design and development of Optical MEMS Pressure Sensor For Pulmonary Ventilator Control based on Fabry Perot interferometry .