Logan Sweeney Email & Phone Number

Texas, United States

Dallas, Texas, United States

Orlando, Florida, United States

Integrated and tested experimental mid-wave infrared threat warning sensors for advanced rotary winged aircraft. Developed program-specific MATLAB scripts to characterize sensor resolution, background discrimination capabilities and field-of-view.Employed Bash and Python to automate data collection for non-uniform correction tables, resulting in a 50% reduction in collection time.Contributed to the analysis of data in vibration and athermalization testing of system components and sensors.Authored detailed test reports derived from data acquired during prior vibration, thermal, and in-flight testing.Drafted finalized testing documentation, which was provided to the customer, ensuring transparency and alignment with project objectives and specifications.Documented interconnect diagrams to illustrate sensor-to-processing unit relationships.Produced comprehensive technical documentation, including finalized testing documentation provided to the customer, serving as essential references and guidelines for test procedures

Orlando, Florida, United States

Acted as design authority on student researched and designed solid, hybrid, and liquid bi-propellant engines.Mentored and guided club members, fostering their growth as engineers and rocket propulsion enthusiasts by providing hands-on experience and educational opportunities.Effectively managed the club's budget and resources, ensuring efficient procurement of materials and equipment for propulsion experiments and projects.Prioritized safety protocols and regulatory compliance in all propulsion-related activities, fostering a culture of responsible experimentation.

Led a team of students in a groundbreaking project, successfully launching the first-ever university developed liquid bipropellant rocket in the state of Florida.Utilized additive manufacturing to design a single-piece nozzle, out of Inconel 718.Preformed cold flow testing of a custom, fuel centered, pintle injector verifying functionality and reliability.Managed the manufacturing of a custom ablative liner tailored to project requirements, preventing motor damage during combustion.Orchestrated the static firing of a Student Research and Design ethanol/N20 liquid rocket motor, producing 200lbf of thrust and 350psi of chamber pressure.Competed in the Friends of Amateur Rocketry Dollar-Per-Foot Challenge reaching an apogee of 4,884ft.

Orlando, Florida, United States

Designed and modeled an “L-class” Student Research and Design solid rocket motor.Used Star-CCM+ to model the flow through a Commercial off-the-shelf nozzle.Lead a small group of members in the design, simulation, and build phase of solid rocket motor.Successfully created and presented a Preliminary Design Review to a board of directors.Static launched a Student Research and Design solid rocket motor to obtain accurate thrust and pressure curves.Competed in the Friends of Amateur Rocketry 51025 competition, reaching an apogee of 5,943ft, and successfully recovering the rocket.

Bachelor Of Science - Bs, Aerospace, Aeronautical And Astronautical Engineering

Minor, Computer Science