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Grant: Discovery Launch Supplement

Concordia University

$12,500.00

Synthesis and experimental combustion studies of gel fuels for advanced propulsion applications

EF 2024-25

Résumé
The demand for energetically improved, reliable, safer, and green propellants for advanced rocket propulsion systems has been constantly increasing over the last few decades. To address these needs, one promising technique involves transforming liquid fuel into a semi-solid gel state. Gel fuels are essentially liquid propellants whose rheological properties are modified by the addition of solid particles called gellants. Additionally, these fuels are safer because of their viscoelastic nature which tends to reduce spillage in the event of leakage. As a result, gel propellants appear to be a promising alternative for various rocket engine systems. However, stable gel fuels are invariably very viscous, difficult to flow, and atomize. These challenges should be addressed in order to develop an efficient gel propulsion rocket engine. Therefore, this research program focuses on developing an innovative thermo-reversible gelation technique for liquid propellants which will overcome the atomization issue while retaining the existing merits of the gel system. To achieve this objective, this research program is structured around four short-term objectives. First, the program will ultimately aim to develop a highly regressive kerosene gel fuel using a low molecular gelator; in the second objective, the research team will establish the thermo-reversible nature of the gel fuels through experimental rheology and microstructural analyses. The third and fourth objectives involve conducting high-pressure ignition and droplet combustion experiments to evaluate the performance of the propellants. The experimental results and analyses obtained throughout this research program will be used to develop a novel design for a gel propulsion rocket engine, intended to overcome the challenges inherent in the existing design. Throughout this program, extensive training will be provided to highly qualified personnel, which includes conducting experiments and numerical modelling, empowering them to cultivate an in-depth understanding of the concepts of advanced rocket propulsion. Furthermore, the work performed will have a direct impact on Canada's commitment to sustainable space exploration and embracing gel propulsion technology can position the Canadian space industry as a world leader in advanced propulsion systems.
Programme
Discovery Launch Supplement
Bénéficiaire
Emplacement
Quebec, Canada
Type de bénéficiaire
Academia
Type
Grant
Source
NSERC's Awards Data

Tel que publié

Application id
DGECR-2024-00194
Name nom
John, Jerin
Department département
Mechanical, Industrial and Aerospace Engineering
Organization id
70
Institution établissement
Concordia University
Province en
Québec
Province fr
Québec
Country en
CANADA
Country fr
CANADA
Fiscal year exercice financier
2024
Competition year année de concours
2024
Award amount
12500
Program id
DGECR
Program name en
Discovery Launch Supplement
Program name fr
Supplément Tremplin vers la découverte
Group en
DISCOVERY RESEARCH
Group fr
RECHERCHE AXÉE SUR LA DÉCOUVERTE
Committee code
1512
Committee name en
Mechanical Engineering
Committee name fr
Génie mécanique
Area of application code
703
Area of application group en
Transportation systems and services
Area of application group fr
Services et systèmes de transport
Area of application en
Aerospace
Area of application fr
Aérospatial
Research subject code
2110
Research subject group en
Mechanical engineering
Research subject group fr
Génie mécanique
Research subject en
Combustion
Research subject fr
Combustion
Field of research list names en
Not available
Field of research list names fr
Non disponible
Socioeconomic objective list names en
Not available
Socioeconomic objective list names fr
Non disponible
Application title
Synthesis and experimental combustion studies of gel fuels for advanced propulsion applications
Keywords
gel propellants; alternative fuels; aerospace propulsion; hypergolic fuels; eco-friendly fuels; rheology; material characterization; ignition; high pressure combustion; droplet combustion
Application summary
The demand for energetically improved, reliable, safer, and green propellants for advanced rocket propulsion systems has been constantly increasing over the last few decades. To address these needs, one promising technique involves transforming liquid fuel into a semi-solid gel state. Gel fuels are essentially liquid propellants whose rheological properties are modified by the addition of solid particles called gellants. Additionally, these fuels are safer because of their viscoelastic nature which tends to reduce spillage in the event of leakage. As a result, gel propellants appear to be a promising alternative for various rocket engine systems. However, stable gel fuels are invariably very viscous, difficult to flow, and atomize. These challenges should be addressed in order to develop an efficient gel propulsion rocket engine. Therefore, this research program focuses on developing an innovative thermo-reversible gelation technique for liquid propellants which will overcome the atomization issue while retaining the existing merits of the gel system. To achieve this objective, this research program is structured around four short-term objectives. First, the program will ultimately aim to develop a highly regressive kerosene gel fuel using a low molecular gelator; in the second objective, the research team will establish the thermo-reversible nature of the gel fuels through experimental rheology and microstructural analyses. The third and fourth objectives involve conducting high-pressure ignition and droplet combustion experiments to evaluate the performance of the propellants. The experimental results and analyses obtained throughout this research program will be used to develop a novel design for a gel propulsion rocket engine, intended to overcome the challenges inherent in the existing design. Throughout this program, extensive training will be provided to highly qualified personnel, which includes conducting experiments and numerical modelling, empowering them to cultivate an in-depth understanding of the concepts of advanced rocket propulsion. Furthermore, the work performed will have a direct impact on Canada's commitment to sustainable space exploration and embracing gel propulsion technology can position the Canadian space industry as a world leader in advanced propulsion systems.