International audienceTo obtain the modelling of an ICP torch that can be used as a test case, we have to determine all the thermodynamic properties and transport coefficients. To calculate the data we have first to determine the composition and the collisions integrals for all the species in the purpose to calculate the transport coefficients. We apply the calculation to the Mars and to the Titan atmosphere compositions. The intensities of the spectral lines are determined versus temperature
The composition and thermal structure of Titan's upper atmosphere are studied between 600 and 2000 k...
International audienceTitan is the largest satellite of Saturn. Its upper atmosphere is well-known f...
International audienceA test case, using a similar methodology and experimental set-up than previous...
International audienceTo obtain the modelling of an ICP torch that can be used as a test case, we ha...
International audienceThe purpose of the work is to make an overview on the results obtained through...
this work is a contribution to the calculation of the transport coefficients for Nitrogen, hydrogen,...
Lors des manoeuvres d'entrée ou d'aérocapture dans l'atmosphère de Titan, une quantité importante d'...
Emission spectroscopy measurements on a plasma representative of Titan atmosphere composition were o...
International audienceThis work is a contribution to the calculation of transport coefficients for n...
This work is a contribution to the calculation of transport coefficients for nitrogen, hydrogen, Ma...
This thesis investigates the modelling of radiating shock layers encountered during atmospheric entr...
La mise en œuvre de missions spatiales demande à développer de nombreuses technologies clés afin de ...
Thermodynamic and transport properties of high temperature Mars atmosphere have been calculated in t...
A new test case, using a quasi-similar methodology and experimental set-up than previous test case 1...
A new test case, using a quasi-similar methodology and experimental set-up than previous test case 1...
The composition and thermal structure of Titan's upper atmosphere are studied between 600 and 2000 k...
International audienceTitan is the largest satellite of Saturn. Its upper atmosphere is well-known f...
International audienceA test case, using a similar methodology and experimental set-up than previous...
International audienceTo obtain the modelling of an ICP torch that can be used as a test case, we ha...
International audienceThe purpose of the work is to make an overview on the results obtained through...
this work is a contribution to the calculation of the transport coefficients for Nitrogen, hydrogen,...
Lors des manoeuvres d'entrée ou d'aérocapture dans l'atmosphère de Titan, une quantité importante d'...
Emission spectroscopy measurements on a plasma representative of Titan atmosphere composition were o...
International audienceThis work is a contribution to the calculation of transport coefficients for n...
This work is a contribution to the calculation of transport coefficients for nitrogen, hydrogen, Ma...
This thesis investigates the modelling of radiating shock layers encountered during atmospheric entr...
La mise en œuvre de missions spatiales demande à développer de nombreuses technologies clés afin de ...
Thermodynamic and transport properties of high temperature Mars atmosphere have been calculated in t...
A new test case, using a quasi-similar methodology and experimental set-up than previous test case 1...
A new test case, using a quasi-similar methodology and experimental set-up than previous test case 1...
The composition and thermal structure of Titan's upper atmosphere are studied between 600 and 2000 k...
International audienceTitan is the largest satellite of Saturn. Its upper atmosphere is well-known f...
International audienceA test case, using a similar methodology and experimental set-up than previous...