For this honors research and senior design project, the authors will research, analyze, and manufacture a rocket motor nozzle for the Akronauts rocket design team. This research and design project will improve how the rocket design team will decide and manufacture nozzles going forward. The impact of this improvement allows the rocket design team to take steps toward being self-sustaining by manufacturing student designed parts as opposed to commercially bought parts. This will not only be successful in increasing student impact on future designs, but also provides a technical challenge for the authors and will present as an impressive feat compared to our competitors at future design competitions. The application of fluid mechanics, thermo...
The nozzle is utilized to change over the compound warm vitality created in the ignition chamber int...
This document details the functionality of a software program used to streamline a rocket propulsion...
This document details the functionality of a software program used to streamline a rocket propulsion...
This paper presents a preliminary nozzle design for a high-altitude rocket to be built by SOAR, the ...
The goal of this project is to design the University of Akron’s first design team built liquid propu...
The nozzle is a major component of a rocket engine, having a significant influence on the overall en...
Several design modifications to commercial off-the-shelf solid rocket motors have been evaluated in ...
The steps in the nozzle design process are examined. The nozzle designer's role in defining design r...
Annular spike nozzle engines have long been the holy grail of rocket engine design, promising superi...
The project\u27s primary goal is to research, design, and manufacture solid rocket motors for compet...
This document outlines the concept, design, and manufacturing stages of the nozzle section to the Ra...
Two nozzles were designed and constructed for testing in the Cal Poly propulsion laboratory to explo...
The University of Alabama’s Aerospace Engineering and Mechanics Department is developing a computati...
As members of The University of Akron’s rocket design team our group designed and fabricated the str...
The cold-gas propulsion system being developed by M-SAT requires improvements to its original nozzle...
The nozzle is utilized to change over the compound warm vitality created in the ignition chamber int...
This document details the functionality of a software program used to streamline a rocket propulsion...
This document details the functionality of a software program used to streamline a rocket propulsion...
This paper presents a preliminary nozzle design for a high-altitude rocket to be built by SOAR, the ...
The goal of this project is to design the University of Akron’s first design team built liquid propu...
The nozzle is a major component of a rocket engine, having a significant influence on the overall en...
Several design modifications to commercial off-the-shelf solid rocket motors have been evaluated in ...
The steps in the nozzle design process are examined. The nozzle designer's role in defining design r...
Annular spike nozzle engines have long been the holy grail of rocket engine design, promising superi...
The project\u27s primary goal is to research, design, and manufacture solid rocket motors for compet...
This document outlines the concept, design, and manufacturing stages of the nozzle section to the Ra...
Two nozzles were designed and constructed for testing in the Cal Poly propulsion laboratory to explo...
The University of Alabama’s Aerospace Engineering and Mechanics Department is developing a computati...
As members of The University of Akron’s rocket design team our group designed and fabricated the str...
The cold-gas propulsion system being developed by M-SAT requires improvements to its original nozzle...
The nozzle is utilized to change over the compound warm vitality created in the ignition chamber int...
This document details the functionality of a software program used to streamline a rocket propulsion...
This document details the functionality of a software program used to streamline a rocket propulsion...