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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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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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