6 projets européens trouvés
Recherche sur 125080 projets européens
TERMINÉ
NEXT GENERATION CERAMIC COMPOSITES FOR COMBUSTION HARSH ENVIRONMENTS AND SPACE (C3HARME)
Date du début: 1 juin 2016, Date de fin: 31 mai 2020,
There is an increasing demand for advanced materials with temperature capability in highly corrosive environments for aerospace. Rocket nozzles of solid/hybrid rocket motors must survive harsh thermochemical and mechanical environments produced by high performance solid propellants (2700-3500°C). Thermal protection systems (TPS) for space vehicles flying at Mach 7 must withstand projected service ...
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12
Participants partenaires
TERMINÉ
TFP Strut Qualification (SPS_TFP_SQ)
Date du début: 1 oct. 2015, Date de fin: 30 sept. 2017,
This proposal aims at qualification by extensive testing of market relevant carbon fibre struts manufactured with the tailored fibre placement (TFP) technology up to TRL 8 for space applications.A strut is a very common structural element in launchers and satellites. The main novelty of the proposed solution is that even the fittings are carbon (state-of-the-art is metal).The requirements and mark ...
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4
Participants partenaires
TERMINÉ
Smart Intelligent Aircraft Structures (SARISTU)
Date du début: 1 sept. 2011, Date de fin: 31 août 2015,
The project proposal concerns the challenges posed by the physical integration of smart intelligentstructural concepts. It addresses aircraft weight and operational cost reductions as well as animprovement in the flight profile specific aerodynamic performance.This concerns material concepts enabling a conformal, controlled distortion of aerodynamicallyimportant surfaces, material concepts enablin ...
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68
Participants partenaires
TERMINÉ
New Robust DESIgn Guideline for Imperfection Sensitive COmposite Launcher Structures (DESICOS)
Date du début: 1 févr. 2012, Date de fin: 31 juil. 2015,
"European Space industry demand for lighter and cheaper launcher transport systems. The proposed project DESICOS contributes to these aims by a new design approach for imperfection sensitive composite launcher structures, exploiting the worst imperfection idea efficiently: the Single Perturbation Load Approach. Currently, imperfection sensitive shell structures prone to buckling are designed accor ...
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13
Participants partenaires
TERMINÉ
Application of tailored fibre placement technology in integral composite structures for ultra-lightweight space applications (SPS_TFP_Strut)
Date du début: 1 oct. 2014, Date de fin: 31 mars 2015,
The project is intended to investigate feasibility of applying the tailored fibre placement (TFP) technology for design and manufacturing of composite structural parts for space applications.One structural element commonly used in load carrying structures for space is the strut. Struts attachment fittings have been impossible to manufacture with lightweight FRP (fibre reinforced polymer) materials ...
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1
Participant partenaire
TERMINÉ
HYBRID ABLATIVE DEVELOPMENT FOR RE-ENTRY IN PLANETARY ATMOSPHERIC THERMAL PROTECTION (HYDRA)
Date du début: 1 févr. 2012, Date de fin: 28 févr. 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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