Northrop Grumman Collaboration Project

Author(s) Information

Dominic De La Mora, California Polytechnic State University, San Luis ObispoFollow
Michael C. Hartley, California Polytechnic State University, San Luis ObispoFollow
Allison Lee, California Polytechnic State University, San Luis ObispoFollow
Chase Pietro, California Polytechnic State University, San Luis ObispoFollow
Seamus Robinson, California Polytechnic State University, San Luis ObispoFollow

College - Author 1

College of Engineering

Department - Author 1

Mechanical Engineering Department

Degree Name - Author 1

BS in Mechanical Engineering

College - Author 2

College of Engineering

Department - Author 2

Mechanical Engineering Department

Degree - Author 2

BS in Mechanical Engineering

College - Author 3

College of Engineering

Department - Author 3

Mechanical Engineering Department

Degree - Author 3

BS in Mechanical Engineering

College - Author 4

College of Engineering

Department - Author 4

Mechanical Engineering Department

Degree - Author 4

BS in Mechanical Engineering

Date

6-2024

Primary Advisor

Hyeonik Song, College of Engineering, Mechanical Engineering Department

Abstract/Summary

The Northrop Grumman Collaboration project, emphasizing the Mechanical Engineering Senior Design team, is focusing on developing the Fire Response Aircraft (FRA) for the autonomous search and rescue system. The goal of this aircraft is to scan a predefined flight path and locate a simulated fire in which other vehicles will respond to the area. This Final Design Review report highlights the overall design, manufacturing, testing, and discussion of the final prototype. Any new changes to the final design since the Critical Design Review report are noted and include appropriate justification. The manufacturing processes for each component are outlined in detail as well as the required steps taken to properly integrate all parts to complete the final prototype. Additionally, testing of the wings, landing gear, and skin adhesion are discussed along with the results to provide verification that the aircraft has met the structural design requirements. Lastly, this document leads into discussion regarding the outcomes of the project and introduces some recommendations and next steps should efforts on the project continue.

URL: https://digitalcommons.calpoly.edu/mesp/753