Author Information

Matthew Karten

Is this project an undergraduate, graduate, or faculty project?

Undergraduate

Project Type

group

Campus

Daytona Beach

Authors' Class Standing

Matthew Karten, Junior Jacob Blanton, Junior Aidan Fogleman, Junior Ryan Meierjohan, Sophomore Timothy Schroeder, Junior

Lead Presenter's Name

Matthew Karten

Lead Presenter's College

DB College of Engineering

Faculty Mentor Name

Lisa Davids

Abstract

Since the inception of rocketry, there has been a clear tradeoff between efficiency and simplicity. The GEM3 Optimized Orbital-class Nozzle engine aims to provide operational efficiency comparable to traditional bipropellant engines while relying on infrastructure similar to monopropellant-based systems. This is achievable through GEM3’s electrical ignition properties and its ability to create a sustained combustion reaction when provided with only a supply of propellant. The main objective of this project is to conduct research and gather data on this propellant’s viability and application for launch vehicles intended to reach Low Earth Orbit (LEO) and beyond. This will be completed over the course of two years during the summer terms of each year by testing its propulsive capabilities on a smaller scale. This project’s primary focus will be to fully construct the proper systems and support structures for a small-scale combustion engine over the course of the second year of this project. Prior to this, two rounds of experiments will be conducted within the first year: Substance Analysis Trials and Combustion Analysis Trials.

Did this research project receive funding support (Spark, SURF, Research Abroad, Student Internal Grants, Collaborative, Climbing, or Ignite Grants) from the Office of Undergraduate Research?

No

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GEM3 Propellant Viability Test

Since the inception of rocketry, there has been a clear tradeoff between efficiency and simplicity. The GEM3 Optimized Orbital-class Nozzle engine aims to provide operational efficiency comparable to traditional bipropellant engines while relying on infrastructure similar to monopropellant-based systems. This is achievable through GEM3’s electrical ignition properties and its ability to create a sustained combustion reaction when provided with only a supply of propellant. The main objective of this project is to conduct research and gather data on this propellant’s viability and application for launch vehicles intended to reach Low Earth Orbit (LEO) and beyond. This will be completed over the course of two years during the summer terms of each year by testing its propulsive capabilities on a smaller scale. This project’s primary focus will be to fully construct the proper systems and support structures for a small-scale combustion engine over the course of the second year of this project. Prior to this, two rounds of experiments will be conducted within the first year: Substance Analysis Trials and Combustion Analysis Trials.

 

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