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ION THRUSTER PERTAINING TO A SPACECRAFT AND METHOD FOR CONTROLLING THE POSITION OF A SPACECRAFT COMPRISING ONE SUCH ION THRUSTER
ION THRUSTER PERTAINING TO A SPACECRAFT AND METHOD FOR CONTROLLING THE POSITION OF A SPACECRAFT COMPRISING ONE SUCH ION THRUSTER
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机译:垂直于航天器的离子推进器和控制包括一个这样的离子推进器的航天器的位置的方法
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摘要
The invention relates to a structure and a method for a drive device pertaining to a space missile comprising at least one ion accelerator arrangement, whereby a neutralising ion source is consciously rendered superfluous and an ion flow with a positive charge excess is expelled. The charge balance is compensated by capturing slow, positively charged particles which are attracted from the environment by a low potential difference, wherefore metallic outer surfaces of the satellite are connected to the cathode or the generator of the ion accelerator arrangement in a galvanically direct or indirect manner.
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