Previous studies carried out by the Aero-Thermo-Mechanics Department at Université Libre de Bruxelles and the Belgium Royal Military academy indicate that Magnesium diboride, MgB2, is a candidate for paraffin-based fuels performance enhancement agent. The main advantage of using Magnesium diboride lies in the fact that this additive is more stable and easier to handle than other metal hydrides, such as Lithium Aluminium Hydride and MgH2. This study presents the results of a series of experimental investigations using the MOUETTE slab burner and the 1kN hybrid rocket motor to characterize the paraffin-fuel samples dopped with MgB2.info:eu-repo/semantics/publishe
Solid fuel ramjets (SFRJ) are known for their operational simplicity and high specific impulse. The ...
This research work aimed at investigating the effects of magnesium metal (powder) and carbon on a po...
Enabling hybrid rocket propulsion to compete with solid and liquid propulsion is the target of the r...
Paraffin-based fuel has a great potential for several innovative missions, including space tourism, ...
Preliminary investigations carried out at the Aero-Thermo-Mechanics Department (ATM) of Université L...
In the framework of EU-project ORPHEE, some innovative solid fuel formulations for hybrid rocket pro...
Hybrid rockets have been intense topic of research for their safety and environmental advantages ove...
Rocket fuels are subjected to intense in-flight inertial, pressure and thermal loads that has drasti...
Solid fuels for hybrid rockets were characterized in the framework of a research ...
The low regression rates for hydroxyl-terminated polybutadiene (HTPB)-based solid fuels and poor mec...
This paper discusses experimental investigations on the effects of innovative micrometer-sized metal...
The purpose of this study is to investigate the use of reactive energetic fuel additives that have t...
In comparison to solid and liquid fueled rockets, hybrids are attractive for their relatively low co...
Experimental investigations have been performed for a lab-scale hybrid rocket motor with hydrogen pe...
The present research describes thermal, rheological and ballistic experimental analyses performed on...
Solid fuel ramjets (SFRJ) are known for their operational simplicity and high specific impulse. The ...
This research work aimed at investigating the effects of magnesium metal (powder) and carbon on a po...
Enabling hybrid rocket propulsion to compete with solid and liquid propulsion is the target of the r...
Paraffin-based fuel has a great potential for several innovative missions, including space tourism, ...
Preliminary investigations carried out at the Aero-Thermo-Mechanics Department (ATM) of Université L...
In the framework of EU-project ORPHEE, some innovative solid fuel formulations for hybrid rocket pro...
Hybrid rockets have been intense topic of research for their safety and environmental advantages ove...
Rocket fuels are subjected to intense in-flight inertial, pressure and thermal loads that has drasti...
Solid fuels for hybrid rockets were characterized in the framework of a research ...
The low regression rates for hydroxyl-terminated polybutadiene (HTPB)-based solid fuels and poor mec...
This paper discusses experimental investigations on the effects of innovative micrometer-sized metal...
The purpose of this study is to investigate the use of reactive energetic fuel additives that have t...
In comparison to solid and liquid fueled rockets, hybrids are attractive for their relatively low co...
Experimental investigations have been performed for a lab-scale hybrid rocket motor with hydrogen pe...
The present research describes thermal, rheological and ballistic experimental analyses performed on...
Solid fuel ramjets (SFRJ) are known for their operational simplicity and high specific impulse. The ...
This research work aimed at investigating the effects of magnesium metal (powder) and carbon on a po...
Enabling hybrid rocket propulsion to compete with solid and liquid propulsion is the target of the r...