7 projets européens trouvés
Recherche sur 125080 projets européens
TERMINÉ
Multi-instrument analysis of Rosetta data – Establishing a new paradigm for cometary activity (MiARD)
Date du début: 1 mars 2016, Date de fin: 31 août 2018,
The MiARD project will use a wide range of data sets from the Rosetta mission (including the Philae lander) to refine the 3D topography of specific areas of comet 67P/Churyumov-Gerasimenko, to study the activity and changes caused by subliming volatiles as the comet nears the Sun, to make inferences about the nature of the top 10 cm of the surface of the comet, to assess whether the landing site o ...
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9
Participants partenaires
TERMINÉ
High Resolution Soil Moisture Mapping (VanderSat)
Date du début: 1 déc. 2015, Date de fin: 31 mai 2016,
... a huge step in this field and is able to bring it down to 100 x 100 meter by using the Copernicus Sentinel Constellation; a staggering improvement of 62.500 times. Within this feasibility study, ATG Europe BV - a recognized as a leading provider of specialized engineering and scientific and technical services to the aerospace, space and high-tech industry - supported by Transmissivity BV - a spec ...
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2
Participants partenaires
TERMINÉ
Composite fuselage section Wafer Design Approach for Safety Increasing in Worst Case Situations and Joints Minimizing (WASIS)
Date du début: 1 janv. 2011, Date de fin: 31 déc. 2014,
"Aeronautics is a key asset for the future of Europe, but nowadays the industry has to face the challenge of “More Affordable, Safer, Cleaner and Quieter” while at the same time accounting for a demand that will triple over the next 20 years. WASIS project aims to rise to this challenge with the development of a composite fuselage structure based on the lattice stiffening concept, optimizing geome ...
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14
Participants partenaires
TERMINÉ
Nose Fuselage/Cockpit Dynamic Characterization for Internal Noise Attenuation (DYNAPIT)
Date du début: 3 févr. 2012, Date de fin: 2 mai 2013,
The research work described in this proposal shall involve detailed simulation of the acoustic performance of CFRP nose fuselage design, and a comparative analysis of a conventional metallic design.The physical properties of CFRP structural components gives a different vibroacoustic response compared to metallic structures. In particular the low material damping and reduced number of mechanical jo ...
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1
Participant partenaire
TERMINÉ
Gas Flows in Micro Electro Mechanical Systems (GASMEMS)
Date du début: 1 oct. 2008, Date de fin: 30 sept. 2012,
Gas flows in microsystems are of great interest for various applications that touch almost every industrial field. This diversity is typified through the following examples: fluidic microactuators for active control of aerodynamic flows, vacuum generators for extracting biological samples, mass flow and temperature micro-sensors, pressure gauges, micro heat-exchangers for the cooling of electronic ...
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14
Participants partenaires
TERMINÉ
HeliconPlasmaHydrazine.COmbinedMicro (HPH.com)
Date du début: 1 déc. 2008, Date de fin: 31 mai 2012,
The objective of the research program is to design, optimize and develop a space plasma thruster based on helicon-radio-frequency technology and its application to a nano-satellite for attitude and position control. Moreover a detailed feasibility study will be also conducted to evaluate the possibility of using the plasma thruster to heat and decompose a secondary propellant. The feasibility stud ...
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15
Participants partenaires
TERMINÉ
Numerical Simulation and Design Optimization of a Lower Fuselage Structure with Advanced Integral Stiffening (FusDesOpt)
Date du début: 1 janv. 2010, Date de fin: 30 juin 2010,
This proposal is for the structural analysis and design optimization of the lower fuselage of an aircraft. The objective of the structural optimization is minimum weight and the design constraints fall into two categories; firstly the capability to withstand structural loads with sufficient margins, and secondly constraints relating to the manufacturing methods. The structure to be optimized is a ...
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