International audienceConsidering more severe operating conditions in combustion chambers, new systems of materials are developed by CNES, ONERA and ICB. In the present study, stabilised hafnia has been chosen for the ceramic part of this system as its thermophysical properties are interesting compared to other ceramics. More precisely, hafnia based materials with different natures (Lu2O3, Y2O3 and Gd2O3) and amounts of stabilisers have been manufactured using a solid state reaction. Fully stabilised materials were obtained and the microstructures and the thermal expansion coefficients up to 1550°C were investigated
The thermal expansion behavior of zirconia ceramics from a given powder type can be tailored withi...
International audienceAccording to the European regulation REACh, a new low-toxicity green propellan...
This study presents first investigations on the high-temperature stability and microstructure evolut...
International audienceConsidering more severe operating conditions in combustion chambers, new syste...
International audienceFor satellite propulsion, new material are developed to sustain harsh thermal ...
International audienceHafnia based ceramics are potential promising candidates to be used as thermal...
International audienceThe needs for space propulsion thruster induce the development of new designs ...
Hafnium carbide powder was synthesized by sol-gel polycondensation of hafnium chloride with citric a...
The current review uses the material requirements of a new space propulsion device, the Variable Spe...
With a melting point in excess of 3000°C and a high density, ultra-high temperature ceramics (UHTCs)...
Aspects of the development and characteristics of thermal shock resistant hafnia ceramic material fo...
Radiation or passively cooled thrust chambers are used for a variety of chemical propulsion function...
The demand for materials that will withstand the high stresses in rapidly rotating parts of the...
Après relecture une erreur est apparue dans le document et doit être retiréInternational audienceThe...
The Italian Aerospace Research Centre (CIRA) is running the National Aerospace Research Program (PRO...
The thermal expansion behavior of zirconia ceramics from a given powder type can be tailored withi...
International audienceAccording to the European regulation REACh, a new low-toxicity green propellan...
This study presents first investigations on the high-temperature stability and microstructure evolut...
International audienceConsidering more severe operating conditions in combustion chambers, new syste...
International audienceFor satellite propulsion, new material are developed to sustain harsh thermal ...
International audienceHafnia based ceramics are potential promising candidates to be used as thermal...
International audienceThe needs for space propulsion thruster induce the development of new designs ...
Hafnium carbide powder was synthesized by sol-gel polycondensation of hafnium chloride with citric a...
The current review uses the material requirements of a new space propulsion device, the Variable Spe...
With a melting point in excess of 3000°C and a high density, ultra-high temperature ceramics (UHTCs)...
Aspects of the development and characteristics of thermal shock resistant hafnia ceramic material fo...
Radiation or passively cooled thrust chambers are used for a variety of chemical propulsion function...
The demand for materials that will withstand the high stresses in rapidly rotating parts of the...
Après relecture une erreur est apparue dans le document et doit être retiréInternational audienceThe...
The Italian Aerospace Research Centre (CIRA) is running the National Aerospace Research Program (PRO...
The thermal expansion behavior of zirconia ceramics from a given powder type can be tailored withi...
International audienceAccording to the European regulation REACh, a new low-toxicity green propellan...
This study presents first investigations on the high-temperature stability and microstructure evolut...