Multi-section type high-efficiency pulse plasma thruster
A pulsed plasma and plasma technology, applied in the field of plasma thrusters, can solve the problems of insufficiency, low energy conversion efficiency, easy failure reliability of ignition starting devices, etc., and achieve the effects of improving acceleration efficiency and reliability.
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[0020] This embodiment discloses a multi-stage high-efficiency pulse plasma thruster. The structure of the thruster is mainly composed of one section of anode 10, one section of cathode 3, two sections of anode 7, two sections of cathode 8, insulating section 5, trigger pole 1, trigger work Composition of mass 2, energy storage capacitor group 11, propellant 4, cladding layer 9 and outer casing 6.
[0021] The thruster has a coaxial structure as a whole, and the electrodes are divided into two sections. The first section of electrodes is mainly used for the process of ablating and ionizing the propellant, and the second section of electrodes is mainly used for the process of plasma acceleration. The first section of electrode consists of a section of anode 10 and a section of cathode 3, both of which are coaxial rings made of brass, wherein the section of anode 10 has an inner diameter of 9 mm, an outer diameter of 10 mm, and a length of 25 mm. A section of cathode 3 has an in...
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