摘要:
Für eine Wanderfeldröhrenanordnung, bei welcher eine Auskoppelanordnung eine über ein Vakuumfenster durch die Vakuumhülle geführte Auskoppelleitung enthält, wird vorgeschlagen, dass die Ausgangsleistung der Verzögerungsleitung (VL) innerhalb der Vakuumhülle (HU) in Teilleistungen aufgeteilt wird, welche auf getrennten Auskoppelleitungen (K1,K2) über getrennte Vakuumfenster (F1,F2) durch die Vakuumhülle zu einer Außenbeschaltung ausgekoppelt werden.
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.
摘要:
The invention relates to various advantageous embodiments of a plasma-accelerator configuration, especially for the configuration and design of electron sources used for ionizing the working gas and/or neutralizing the discharged plasma jet.
摘要:
The invention relates to an ion accelerator arrangement comprising an electrostatic acceleration field between a cathode to which a frame potential is applied and an anode to which a high-voltage potential is applied. Said ion accelerator arrangement further comprises a gas supply system into which a gas-permeable, open porous insulator member is introduced. Also described is a high-voltage insulator arrangement that comprises such an insulator member and is suitable, inter alia, for such an ion accelerator arrangement and for the corona-resistant insulation of other components to which a high voltage is applied.
摘要:
The invention relates to a drive arrangement in a spacecraft, comprising several drive units (TW1,TW2,TW3), several individually controllable drive units that can be continuously applied to a common, constant voltage potential (HV), and a control of the axial thrust in the respective drive units is achieved due to the fact that the production of plasma in the respective drive units is individually controlled. In particular, the time-variable control of the production of plasma occurs by the time-variable control of the flow of neutral working gas (AG) in the ionisation chamber (IK).
摘要:
The invention relates to a plasma accelerator arrangement, especially for use as an ion thruster in a spacecraft. According to the invention, the arrangement is structured in such a way that an accelerated electron beam is introduced into an ionisation chamber with propellant gas and guided through the ionisation chamber as a concentrated beam, towards an electric deceleration field which also acts as an acceleration field for the propellant ions produced by ionisation. The arrangement produces a focussed beam of an essentially neutral plasma with a high degree of efficiency. Examples of configurations for electric and magnetic fields for guiding and focussing the beams are also given.
摘要:
The invention relates to a multistage plasma accelerator system that comprises at least one intermediate electrode between the plasma chamber between electrodes that include each other. An especially good efficiency can be achieved by way of an uneven distribution of potential to the potential stages formed by the plurality of electrodes having a high potential gradient of the last stage, when the plasma beam emerges, and by a special shape of the magnetic field prevailing in the plasma chamber of the last stage.
摘要:
The invention relates to a multistage plasma accelerator system that comprises at least one intermediate electrode between the plasma chamber between electrodes that include each other. An especially good efficiency can be achieved by way of an uneven distribution of potential to the potential stages formed by the plurality of electrodes having a high potential gradient of the last stage, when the plasma beam emerges, and by a special shape of the magnetic field prevailing in the plasma chamber of the last stage.