College

College of Engineering and Polymer Science

Date of Last Revision

2026-05-06 06:30:38

Major

Aerospace Systems Engineering

Honors Course

AESE497

Number of Credits

2

Degree Name

Bachelor of Science

Date of Expected Graduation

Spring 2026

Abstract

This project seeks to bring new testing capability to the Zips Aero Design Team through the design, manufacture, integration, and testing of a dynamic thrust testbed for UAV electric motors. The project centers upon the revival and modification of a past prototype aircraft for use as a testbed for in-flight thrust measuring and recording. The team currently lacks the ability to test dynamic thrust under the operating conditions and flight speeds that are encountered in competition. Project technical areas include component and product design, electrical and electronics, and fluid mechanics, including the use of SolidWorks, MATLAB, and ArduPilot. Aside from the work that will be done on the components of the candidate aircraft that need repaired or upgraded, the major addition will be a universal motor mount fixture, allowing a wide range of motors with different bolt patterns to be tested. Onboard systems measure thrust in conjunction with other flight information such as airspeed, groundspeed, and atmospheric conditions to show the relationship between these variables.

Research Sponsor

Dr. Nicholas Garafolo

First Reader

Dr. Jonathan Mackey

Second Reader

Mr. Solomon Whitmire

Honors Faculty Advisor

Dr. Scott Sawyer

Proprietary and/or Confidential Information

No

Community Engaged Scholarship

No

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