I focus on propulsion component selection for deep space satellite systems and support Blue Origin's Human Landing System (HLS) program through Lockheed Martin's CIS Lunar Transporter vehicle. My role includes requirement verification and analysis for propulsion components like hypergolic thrusters and liquid/gas filters.A key part of my work involves developing software tools to automate and optimize data processing for thruster qualification and acceptance tests, allowing for more efficient handling of large datasets. I’ve also created a parametric vehicle model in MATLAB to track contamination flow across various systems and vehicles for a multi-vehicle lunar mission, providing useful insights to help manage component protection and overall system performance while allowing for system design changes.

Propulsion Engineering Intern focused on deep space monopropellant missions. Developed procedures and conducted tests to assess the performance of additively manufactured filters, providing critical insights to inform manufacturing design.

As a volunteer board member of the Arapahoe Rescue Patrol, a Colorado-based Search & Rescue team comprised entirely of high school students, I develop technical solutions to enhance fundraising efforts and secure essential resources for the team. My role also emphasizes youth development, ensuring members have the support they need to cultivate their first responder skills.

Developed and maintained support for website content and online member applications to improve the organization's online presence and functionality.

As an officer, I led multi-team search, technical rescue, and recovery operations in collaboration with local and federal emergency services.

Across 4 different semesters, I assisted in teaching classes in electronics and communications, dynamics and control, and thermodynamics and aerodynamics. During this time I assisted in instructing lab courses, hosting office hours, and proctor exams.

Led the software and electronics architecture for the "Spice Shuttle", a kerolox liquid engine flight vehicle. Provided system analysis, requirements, and integration support. Additionally led the development of a high-precision capacitive fuel sensor and a flow control valve for a liquid rocket turbopump.