A Strategy to Characterize the LISA-Pathfinder Cold Gas Thruster System
| Data(s) |
2015
|
|---|---|
| Resumo |
The cold gas micro-propulsion system that will be used during the LISA-Pathfinder mission will be one of the most important component used to ensure the "free-fall" of the enclosed test masses. In this paper we present a possible strategy to characterize the effective direction and amplitude gain of each of the 6 thrusters of this system. |
| Identificador | |
| Idioma(s) |
eng |
| Publicador |
Bristol : IOP Publishing Ltd. |
| Relação |
http://dx.doi.org/10.1088/1742-6596/610/1/012026 ISSN:1742-6588 ESSN:1742-6596 |
| Direitos |
CC BY 3.0 https://creativecommons.org/licenses/by/3.0/de/ frei zugänglich |
| Fonte |
10th International LISA Symposium, May 18-23, 2014, Gainesville, Florida Journal of Physics Conference Series 610 (2015) |
| Palavras-Chave | #LISA Pathfinder #Astronomy #Astrophysics #Physics, Applied #ddc:500 #ddc:530 |
| Tipo |
status-type:publishedVersion doc-type:article doc-type:conferenceObject doc-type:Text |