4 European Projects Found
Searched on 125080 European Projects
FINISHED
High-frequency ELectro-Magnetic technologies for advanced processing of ceramic matrix composites and graphite expansion (HELM)
Start date: Jun 1, 2012, End date: May 31, 2016,
"Lightweight ceramics and fibre reinforced ceramic composites, such as non-oxide Ceramic Matrix Composites (CMCs) and Expanded Graphite (EG), represent very promising solutions for high temperature applications in strategic industrial sectors, such as transport and energy. In fact, these materials are one of topical priorities of the European Technology Platform EuMAT and a strategic issue of the ...
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21
Partners Participants
FINISHED
INNOVATIVE THERMAL MANAGEMENT CONCEPTS FOR THERMAL PROTECTION OF FUTURE SPACE VEHICLES (THOR)
Start date: Jan 1, 2013, End date: Dec 31, 2015,
There are key space technologies existing at European level and during the last space calls many European projects are framed on space re-entry, but none of them dealing with radically new technologies, able to compete with technologies from other leading countries or allowing collaboration with them. The THOR project will provide knowledge in key space technologies for accessing space, through th ...
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9
Partners Participants
FINISHED
HYBRID ABLATIVE DEVELOPMENT FOR RE-ENTRY IN PLANETARY ATMOSPHERIC THERMAL PROTECTION (HYDRA)
Start date: Feb 1, 2012, End date: Feb 28, 2015,
The aim of this proposal is the development of TPS for their use in space applications with extreme oxidative environments and high temperature resistance, such as hot parts of space vehicles for orbital entry (ARV), planetary probes and NEO exploration. Previous studies on ARV vehicle have shown that TPS hybrid systems based on ablators integrated with thermo-structural materials are good candida ...
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12
Partners Participants
FINISHED
MULTIFUNCTIONAL COMPONENTS FOR AGRESSIVE ENVIROMENTS IN SPACE APPLICATIONS (SMARTEES)
Start date: Jan 1, 2011, End date: Dec 31, 2013,
"The aim of this proposal is the development of ceramic composites structures which are needed for applications in aggressive environments, where (oxidative) and temperatures are required, such as hot parts of space vehicles for orbital re-entry (reusable launcher vehicles, RLVs). The solution will be focused on re-usable systems.As expressed by the European Commission a non-dependent access to th ...
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