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Satellites having such thrusters, as well as how to stop the electric engine of such a thruster in electrical and thruster

机译:具有此类推进器的卫星,以及如何在电气和推进器中停止此类推进器的电动机

摘要

The valve (5, 6) electric thrusters of the present invention, the system for supplying the electric power engine have high-pressure tank (10), the ionizable gas electric engine of one (1) at least, the high-pressure tank (1 I have a pipeline system for carrying (40) and cathode (26) anode electrical engine low pressure buffer tank (2) and gas (2) low pressure buffer tank that is connected to). Low pressure buffer tank (2) has an opening for the connecting part (10) electric engine. Thruster comprises a means for detecting the intensity of the emission current between the anode (26) and cathode (40) is smaller than the threshold value, blocking the release voltage Following this detection. The use in satellites.
机译:本发明的阀(5、6)电动推进器,用于向电力发动机供应的系统具有高压罐(10),至少一个(1)的可电离气体电动发动机,高压罐(图1I具有用于承载(40)和阴极(26)阳极电动发动机低压缓冲罐(2)和与之连接的气体(2)低压缓冲罐的管道系统。低压缓冲箱(2)具有用于电动发动机的连接部分(10)的开口。推力器包括用于检测阳极(26)和阴极(40)之间的发射电流的强度小于阈值,从而在该检测之后阻止释放电压的装置。在卫星上的使用。

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