A5014215161- Rocket and propulsion systems research
- Energetic Materials and Combustion
- Electrohydrodynamics and Fluid Dynamics
- Spacecraft Design and Technology
- Plasma Diagnostics and Applications
- Microfluidic and Bio-sensing Technologies
- Organic Electronics and Photovoltaics
- Conducting polymers and applications
- Molecular Junctions and Nanostructures
- Perovskite Materials and Applications
- Microfluidic and Capillary Electrophoresis Applications
- Diamond and Carbon-based Materials Research
- Electron and X-Ray Spectroscopy Techniques
- Boron and Carbon Nanomaterials Research
- Electrical and Bioimpedance Tomography
- Acoustic Wave Phenomena Research
- Mechanical and Optical Resonators
- Advancements in Photolithography Techniques
- Force Microscopy Techniques and Applications
- Speech and Audio Processing
- Gas Dynamics and Kinetic Theory
- Music Technology and Sound Studies
- Advanced MEMS and NEMS Technologies
- Nonlocal and gradient elasticity in micro/nano structures
- Material Properties and Applications
Franche-Comté Électronique Mécanique Thermique et Optique - Sciences et Technologies
2019-2022
Université de Bourgogne
2020
Centre National de la Recherche Scientifique
2005-2020
UniLaSalle Amiens (ESIEE-Amiens)
2015
Badji Moktar-Annaba University
2012-2015
Université Gustave Eiffel
2015
University of Laghouat
2015
Laboratoire d'Analyse et d'Architecture des Systèmes
2005-2008
Roche (France)
2005
With the aim of selecting particular frequencies interest and rejecting others, waveguiding filtering properties a two-dimensional phononic crystal slab are investigated in context application. To this end, we designed manufactured metallic device that consists square lattice cylindrical pillars mounted on top plate by using 3D printing technology. We respectively explored theoretical experimental characteristics finite element method, Micro System Analyzer (MSA) scanning laser Doppler...
Since combustion is an easy way to achieve large quantities of energy from a small volume, we developed MEMS based solid propellant microthruster array for spacecraft and micro-air-vehicle applications. A thruster composed fuel chamber layer, top-side igniter with micromachined nozzle in the same silicon layer. Layers are assembled by adhesive bonding give final array. The thrust force generated stored few millimeter cube chamber. micro-igniter polysilicon resistor deposited on low stress...
A combined theoretical and experimental investigation of the electronic structure optical properties poly(3-hexylthiophene) (P3HT), poly[3-(4-octylphenyl)thiophene] (POPT) poly[3-(4-octylphenoxy)thiophene] (POPOT) is reported. In comparison with P3HT, POPT POPOT exhibit better stabilities presence an oxygen atom and/or a phenyl ring in side chains enhances conjugation. Quantum chemical calculations have been performed on oligomers increasing chain length to establish changes when going from...
Solid propellant micro-thruster is an alternative option to cold gas and field emission electric propulsion systems for space. It can also be used autonomous Micro-Air-Vehicles (MAV) micro-propulsion in complement electrical motor. simple, cheap requires low power ignite the micro-combustion of a few milli-grammes solid propellant. This paper presents two concepts micro-thruster. The first one sandwich three parts: combustion chamber (with or several wafers), igniter convergent-divergent...