Abstract
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.
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CITATION STYLE
APA
Armano, M., Audley, H., Auger, G., Baird, J., Binetruy, P., Born, M., … Zweifel, P. (2015). A Strategy to Characterize the LISA-Pathfinder Cold Gas Thruster System. In Journal of Physics: Conference Series (Vol. 610). Institute of Physics Publishing. https://doi.org/10.1088/1742-6596/610/1/012026
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