Led the design of a spacecraft to carry out the mission's science objectives, specifically the development of the Thermal subsystem
Researched similar mission's architecture for any heritage subsystems that could be utilized to increase the design's confidence
Performed trade studies between subsystem architectures to determine which would best satisfy the mission's science objectives while maintaining awareness of the mission's design constraints for mass, power, cost, and schedule
Demonstrated knowledge by following the NASA mission life cycle, up to submission of a Preliminary Design Review, for a robotic space mission
RESEARCH INTERN
Missouri NASA Space Grant Consortium
05.2024 - 08.2024
Committed over 400 hours to the university M-SAT team, focusing on a variety of tasks related to the propulsion, thermal, and power subsystem
Modeled aluminum honeycomb solar panels in Thermal Desktop, performed thermal node analysis with lumped material properties, and assisted with modelling board stack components
Researched cold gas propulsion system using R134-a, configured coding for system control in Arduino Mega, and worked on the electronics setup for the prop system
DRIVETRAIN & CHASSIS MEMBER - HELIOS
Mars Rover Design Team
09.2023 - 03.2024
Revised the auto-box design to ensure compatibility with new arm system of rover using French cleat bars
Created new camera shrouds for ZED 2i Mini cameras due to new orientation in Siemens NX
Assisted with the design of battery box for the rover, and machined internal components in SDELC shop
Education
Bachelor of Science - Aerospace Engineering
Missouri University of Science And Technology
Rolla, MO
05-2027
Skills
THERMAL DESKTOP
MATLAB
KICAD
SCIENCE TRACEABILITY MATRIX
SIEMENS NX
AUTOCAD
SOLIDWORKS
MANUAL MILL & LATHE
ARDUINO
LABVIEW
Relevant Classwork
Thermodynamics | Dynamics | Mechanics of Material | Spacecraft Design | Aircraft Design | Differential Equation | Heat Transfer | Aircraft Vehicle Performance