Study of Combustion Mechanisms and Optimization of Iron- and Lunar Regolith-Based Pyrotechnic Compositions for Space Applications // Study of Combustion Mechanisms and Optimization of Iron- and Lunar Regolith-Based Pyrotechnic Compositions for Space Appli
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ABG-139752
ADUM-76048 |
Sujet de Thèse | |
| 04/07/2026 |
Université d'Orléans
ORLEANS - Centre Val de Loire - France
Study of Combustion Mechanisms and Optimization of Iron- and Lunar Regolith-Based Pyrotechnic Compositions for Space Applications // Study of Combustion Mechanisms and Optimization of Iron- and Lunar Regolith-Based Pyrotechnic Compositions for Space Appli
- Electronique
combustion, pyroytechnic compositons, lunar regolith
combustion, pyroytechnic compositons, lunar regolith
combustion, pyroytechnic compositons, lunar regolith
Description du sujet
Subject Description
Context and Issues:
Future lunar and Martian space missions will require autonomous energy systems capable of producing heat in situ, without relying on an atmosphere. Pyrotechnic compositions—energetic materials that can burn without atmospheric oxygen—offer a promising solution, but their development for space applications is currently limited by two scientific challenges:
1. Understanding the physico-chemical mechanisms governing the ignition and combustion of iron/regolith mixtures, especially in the condensed phase.
2. The lack of predictive models for designing controlled combustion systems suited to the constraints of long-duration missions.
Scientific Objectives:
This thesis aims to (i) experimentally characterize the combustion of composite iron/lunar regolith pellets, investigating the influence of various parameters on combustion rate (porosity, particle size, potential additives such as Mg), (ii) develop a phenomenological model correlating the structural properties of the mixtures (analyzed via electron microscopy) with their energetic performance (combustion rate, ignition energy), and (iii) validate this model through controlled environment tests (constant volume reactor, high-speed camera, photodiodes, and pyrometry).
This work will contribute to advancing ISRU (In-Situ Resource Utilization) technologies by proposing a sustainable energy solution based on materials available in situ.
Methodology
The thesis will involve (i) manufacturing pyrotechnic composition pellets with varying compositions and compaction pressures, (ii) characterization campaigns for thermal (mass, heat flux, transport properties), structural (electron microscopy), and energetic (combustion rates, ignition energies via Langlie method) analysis, and (iii) numerical modeling of combustion phenomena, with experimental validation.
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Subject Description
Context and Issues:
Future lunar and Martian space missions will require autonomous energy systems capable of producing heat in situ, without relying on an atmosphere. Pyrotechnic compositions—energetic materials that can burn without atmospheric oxygen—offer a promising solution, but their development for space applications is currently limited by two scientific challenges:
1. Understanding the physico-chemical mechanisms governing the ignition and combustion of iron/regolith mixtures, especially in the condensed phase.
2. The lack of predictive models for designing controlled combustion systems suited to the constraints of long-duration missions.
Scientific Objectives:
This thesis aims to (i) experimentally characterize the combustion of composite iron/lunar regolith pellets, investigating the influence of various parameters on combustion rate (porosity, particle size, potential additives such as Mg), (ii) develop a phenomenological model correlating the structural properties of the mixtures (analyzed via electron microscopy) with their energetic performance (combustion rate, ignition energy), and (iii) validate this model through controlled environment tests (constant volume reactor, high-speed camera, photodiodes, and pyrometry).
This work will contribute to advancing ISRU (In-Situ Resource Utilization) technologies by proposing a sustainable energy solution based on materials available in situ.
Methodology
The thesis will involve (i) manufacturing pyrotechnic composition pellets with varying compositions and compaction pressures, (ii) characterization campaigns for thermal (mass, heat flux, transport properties), structural (electron microscopy), and energetic (combustion rates, ignition energies via Langlie method) analysis, and (iii) numerical modeling of combustion phenomena, with experimental validation.
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Début de la thèse : 01/10/2026
Context and Issues:
Future lunar and Martian space missions will require autonomous energy systems capable of producing heat in situ, without relying on an atmosphere. Pyrotechnic compositions—energetic materials that can burn without atmospheric oxygen—offer a promising solution, but their development for space applications is currently limited by two scientific challenges:
1. Understanding the physico-chemical mechanisms governing the ignition and combustion of iron/regolith mixtures, especially in the condensed phase.
2. The lack of predictive models for designing controlled combustion systems suited to the constraints of long-duration missions.
Scientific Objectives:
This thesis aims to (i) experimentally characterize the combustion of composite iron/lunar regolith pellets, investigating the influence of various parameters on combustion rate (porosity, particle size, potential additives such as Mg), (ii) develop a phenomenological model correlating the structural properties of the mixtures (analyzed via electron microscopy) with their energetic performance (combustion rate, ignition energy), and (iii) validate this model through controlled environment tests (constant volume reactor, high-speed camera, photodiodes, and pyrometry).
This work will contribute to advancing ISRU (In-Situ Resource Utilization) technologies by proposing a sustainable energy solution based on materials available in situ.
Methodology
The thesis will involve (i) manufacturing pyrotechnic composition pellets with varying compositions and compaction pressures, (ii) characterization campaigns for thermal (mass, heat flux, transport properties), structural (electron microscopy), and energetic (combustion rates, ignition energies via Langlie method) analysis, and (iii) numerical modeling of combustion phenomena, with experimental validation.
------------------------------------------------------------------------------------------------------------------------------------------------------------------------
------------------------------------------------------------------------------------------------------------------------------------------------------------------------
Subject Description
Context and Issues:
Future lunar and Martian space missions will require autonomous energy systems capable of producing heat in situ, without relying on an atmosphere. Pyrotechnic compositions—energetic materials that can burn without atmospheric oxygen—offer a promising solution, but their development for space applications is currently limited by two scientific challenges:
1. Understanding the physico-chemical mechanisms governing the ignition and combustion of iron/regolith mixtures, especially in the condensed phase.
2. The lack of predictive models for designing controlled combustion systems suited to the constraints of long-duration missions.
Scientific Objectives:
This thesis aims to (i) experimentally characterize the combustion of composite iron/lunar regolith pellets, investigating the influence of various parameters on combustion rate (porosity, particle size, potential additives such as Mg), (ii) develop a phenomenological model correlating the structural properties of the mixtures (analyzed via electron microscopy) with their energetic performance (combustion rate, ignition energy), and (iii) validate this model through controlled environment tests (constant volume reactor, high-speed camera, photodiodes, and pyrometry).
This work will contribute to advancing ISRU (In-Situ Resource Utilization) technologies by proposing a sustainable energy solution based on materials available in situ.
Methodology
The thesis will involve (i) manufacturing pyrotechnic composition pellets with varying compositions and compaction pressures, (ii) characterization campaigns for thermal (mass, heat flux, transport properties), structural (electron microscopy), and energetic (combustion rates, ignition energies via Langlie method) analysis, and (iii) numerical modeling of combustion phenomena, with experimental validation.
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Début de la thèse : 01/10/2026
Nature du financement
Précisions sur le financement
Programmes gouvernementaux hors France et Union Européenne
Présentation établissement et labo d'accueil
Université d'Orléans
Etablissement délivrant le doctorat
Université d'Orléans
Ecole doctorale
552 Energie, Matériaux, Sciences de la Terre et de l'Univers - EMSTU
Profil du candidat
Master's degree in mechanical engineering or energetics. Interest in experimental work, Excellent command of English in speaking and writing, Personal initiative, reliability, teamwork and communication skills
Master's degree in mechanical engineering or energetics. Interest in experimental work, Excellent command of English in speaking and writing, Personal initiative, reliability, teamwork and communication skills
Master's degree in mechanical engineering or energetics. Interest in experimental work, Excellent command of English in speaking and writing, Personal initiative, reliability, teamwork and communication skills
31/07/2026
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