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DRIVE DEVICE PERTAINING TO A SPACE MISSILE AND METHOD FOR CONTROLLING THE POSITION OF A SPACE MISSILE COMPRISING ONE SUCH DRIVE DEVICE
DRIVE DEVICE PERTAINING TO A SPACE MISSILE AND METHOD FOR CONTROLLING THE POSITION OF A SPACE MISSILE COMPRISING ONE SUCH DRIVE DEVICE
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机译:与空间导弹有关的驱动设备以及用于控制包括一个这样的驱动设备的空间导弹的位置的方法
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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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