Electrons emitted on spacecraft surfaces can generate negative potential barriers. This may affect the equilibrium potential of the spacecraft, which can be driven more negative and jeopardise plasma measurements by repelling low energy particles. This phenomenon is investigated with the help of a numerical method based on the turning point formalism to classify orbits and which is validated with a PIC code. Comparison with spacecraft data in the magnetosphere is performed
International audienceA three-dimensional, self-consistent code is employed to solve for the static ...
International audienceIn this paper, the electrostatic sheath of a simplified spacecraft is investig...
International audienceIn this paper, the electrostatic sheath of a simplified spacecraft is investig...
Electrons emitted on spacecraft surfaces can generate negative potential barriers. This may affect t...
Electrons emitted on spacecraft surfaces can generate negative potential barriers. This may affect t...
Electrons emitted on spacecraft surfaces can generate negative potential barriers. This may affect t...
In this paper, a fully self-consistent model of the plasma around an electron emitting central body ...
Plasma and field measurements on board magnetospheric spacecraft can be influenced by the spacecraft...
Plasma and field measurements on board magnetospheric spacecraft can be influenced by the spacecraft...
Plasma and field measurements on board magnetospheric spacecraft can be influenced by the spacecraft...
Low-energy secondary electrons have been observed to be reflected back to the spacecraft during ecli...
Low-energy secondary electrons have been observed to be reflected back to the spacecraft during ecli...
Low-energy secondary electrons have been observed to be reflected back to the spacecraft during ecli...
Low-energy secondary electrons have been observed to be reflected back to the spacecraft during ecli...
International audienceA three-dimensional, self-consistent code is employed to solve for the static ...
International audienceA three-dimensional, self-consistent code is employed to solve for the static ...
International audienceIn this paper, the electrostatic sheath of a simplified spacecraft is investig...
International audienceIn this paper, the electrostatic sheath of a simplified spacecraft is investig...
Electrons emitted on spacecraft surfaces can generate negative potential barriers. This may affect t...
Electrons emitted on spacecraft surfaces can generate negative potential barriers. This may affect t...
Electrons emitted on spacecraft surfaces can generate negative potential barriers. This may affect t...
In this paper, a fully self-consistent model of the plasma around an electron emitting central body ...
Plasma and field measurements on board magnetospheric spacecraft can be influenced by the spacecraft...
Plasma and field measurements on board magnetospheric spacecraft can be influenced by the spacecraft...
Plasma and field measurements on board magnetospheric spacecraft can be influenced by the spacecraft...
Low-energy secondary electrons have been observed to be reflected back to the spacecraft during ecli...
Low-energy secondary electrons have been observed to be reflected back to the spacecraft during ecli...
Low-energy secondary electrons have been observed to be reflected back to the spacecraft during ecli...
Low-energy secondary electrons have been observed to be reflected back to the spacecraft during ecli...
International audienceA three-dimensional, self-consistent code is employed to solve for the static ...
International audienceA three-dimensional, self-consistent code is employed to solve for the static ...
International audienceIn this paper, the electrostatic sheath of a simplified spacecraft is investig...
International audienceIn this paper, the electrostatic sheath of a simplified spacecraft is investig...