College

College of Engineering and Polymer Science

Date of Last Revision

2025-04-29 12:39:25

Major

Aerospace Systems Engineering

Honors Course

AESE 497

Number of Credits

2

Degree Name

Bachelor of Science

Date of Expected Graduation

Spring 2025

Abstract

An electronically actuated pressure-regulation valve and controller are necessary for maintaining pressure levels in a pressure-fed liquid-fueled rocket engine. Mechanical regulators are too heavy and have unacceptably high-pressure variation throughout the operation of a dynamic system like a rocket. Developing an electronic pressure regulator using a PID controller is a method by which a reliable, accurate, and lightweight flow regulator can be built for use on a rocket vehicle. This work will outline the development of flow simulations, PID controller, physical valve hardware, and initial testing.

Research Sponsor

Dr. Manigandan Kannan

First Reader

Dr. Nicholas Garafolo

Second Reader

Alex Povitsky

Honors Faculty Advisor

Scott Sawyer

Proprietary and/or Confidential Information

No

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