Projects & Research

STRATOS (Simulation of Thrust, Rate-of-climb, Aerodynamics, and Total Operating States) is a High-Fidelity Aircraft Performance & Envelope Simulation Environment. This physics-based flight performance simulator enables preliminary aerospace engineering analysis, modeling subsonic aircraft performance using first-principles aerodynamic and propulsion equations. Engineers can test whether proposed aircraft configurations meet mission requirements, with outputs including performance plots, flight envelope analysis, and key metrics. The system features four integrated subsystems: Atmospheric Condition & Standard Earth Systems (ACES), Raw Logistic Modulator (RLM), Optimal Statistics Calculator (OSC), and Report Summarizer (RS).

Developed a comprehensive US Patent-Pending spacecraft design to address the critical and growing problem of space debris proliferation in Earth's orbit. The solution includes a novel debris capture mechanism, propulsion system optimization for orbital maneuvers, and a detailed algorithm governing system operations from debris identification through capture and deorbit sequences. This project represents the intersection of orbital mechanics, spacecraft design, and mission planning to create a practical solution for one of the most pressing challenges in space sustainability.