United States
I am an incoming aerospace engineering student focused on advanced propulsion, high-performance engineering systems, and developing transformative technologies. My primary research interest is rotating detonation engines, where I have conducted independent research analyzing combustor architectures, performance tradeoffs, and system reliability. Beyond research, I design and build high-performance model rockets with integrated telemetry and recovery systems, applying principles of aerodynamics, structures, and systems engineering. I also lead Next-Gen Rocketry, expanding access to hands-on aerospace education. Long term, I aim to combine deep technical expertise with entrepreneurship to build and scale next-generation aerospace technologies.
Designed, simulated, built, and tested multiple high-performance model rockets with telemetry and dual deployment to deepen my understanding of aerodynamics, propulsion, and systems engineering. Integrated sustainable materials, custom CAD components, onboard data-logging systems. Applied principles of aerospace engineering, including thrust modeling, center-of-pressure alignment, and fin optimization, while iterating through full design–build–test cycles. These projects strengthened my technical skills in physics, electronics, and prototyping and laid the foundation for my work in aerospace engineering.
I lead Next-Gen Rocketry, a free STEM education initiative funded by the National Association of Rocketry (NAR) that teaches sustainable rocketry and aerospace fundamentals through hands-on activities to NYC schools and community centers in underserved areas. Having taught over 1000+ kids across NYC, I’ve introduced elementary and middle-school students to physics and engineering principles using model rockets and simple materials. Our goal is to make STEM accessible and exciting for all kids, regardless of background, and to inspire them to dream big and boldly. Learn more: https://aerospace79.wpcomstaging.com/next-gen-rocketry-workshop/
Conducted an in-depth literature review on comparing the relatively new hollow combustor with conventional annular combustors in rotary detonation engines in terms of performance and operational reliability for practical applications. Potential solutions to mitigate performance deficits in the hollow combustor are also proposed. Paper published in the NHSJS: https://nhsjs.com/2026/comparative-performance-analysis-of-hollow-and-annular-combustors-in-rotating-detonation-engines/.
Designed and modeled a custom extruder for a low-cost large-format 3D printer prototype with a build volume of 800×800×1000 mm and total cost under $500, optimizing for functionality and manufacturability. Collaborated with a team of interns on mechanical assembly integration, improving structural efficiency and usability. Reduced costs ~67% and production time ~90% by replacing imported parts with in-house 3D-printed components, enhancing prototype accessibility for schools, makers, and small businesses.
Research project on using sustainable hydrogen fuel for promising propulsion technology called rotary detonation engines. Presented to 200+ students and faculty in auditorium. Ranked top 3. Invited to Geological Society of America Conference. Presented at York College in JFK Aviation & Aeronautics Program.