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A Magnetoplasma Thruster with Conical Porous Hollow Cathode

A magnetic plasma and hollow cathode technology, applied in the field of electric propulsion, can solve the problems affecting the operation of the thruster, structural damage, changes, etc., and achieve the effects of improving current emission capability, uniform wall thickness, and preventing loosening

Active Publication Date: 2018-09-11
BEIHANG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

If its structural design is unreasonable, it is likely to cause structural damage or change due to high temperature, which will affect the work of the thruster

Method used

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  • A Magnetoplasma Thruster with Conical Porous Hollow Cathode
  • A Magnetoplasma Thruster with Conical Porous Hollow Cathode
  • A Magnetoplasma Thruster with Conical Porous Hollow Cathode

Examples

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Embodiment Construction

[0031] The present invention will be described in further detail below.

[0032] The present invention has a kind of magnetic plasma thruster with conical porous hollow cathode, such as figure 1 As shown, it includes an anode 1 , a cathode 2 , an insulator 3 , a first cathode connector 4 , a second cathode connector 5 , an intermediate connector 6 , an insulating sleeve 7 and an anode connector 8 .

[0033] The magnetoplasma thruster has a cylindrical structure as a whole, such as figure 2 and image 3 As shown, the exterior includes from left to right: intermediate connector 6, anode connector 8 and anode 1;

[0034] The middle connector 6 is located at the leftmost end of the magnetic plasma thruster, and it is a disc structure with a hole in the middle. Six insulating sleeves 7 are symmetrically installed on the disc, and each insulating sleeve 7 is connected to the anode connector 8 by screws. , so that there is a gap between the anode connecting piece 8 and the interm...

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Abstract

The invention discloses a magnetic plasma thruster provided with a conical porous hollow cathode and belongs to the electric propulsion field. The magnetic plasma thruster provided with the conical porous hollow cathode is of a cylindrical structure as a whole. The exterior of the magnetic plasma thruster provided with the conical porous hollow cathode sequentially comprises a middle connection piece, an anode connection piece and an anode from left to right. The anode connection piece is connected with the anode and the middle connection piece at the same time. The interior of the magnetic plasma thruster provided with the conical porous hollow cathode sequentially comprises a second cathode connection piece, a first cathode connection piece, an insulator and the cathode from left to right, and the second cathode connection piece, the first cathode connection piece, the insulator and the cathode are coaxially matched; the second cathode connection piece is provided with the first cathode connection piece in a matched manner in the radial direction; the insulator is arranged in the anode connection piece in a clamped and sleeved manner; the cathode is clamped to the insulator and the conical face of the first cathode connection piece; and the conical face of the cathode and the conical face of the first cathode connection piece are closely matched through a 5-degree conical angle. The magnetic plasma thruster provided with the conical porous hollow cathode has the beneficial effects that the cathode is wrapped in the cathode connection pieces, the second cathode connection piece tightly presses the tail portion of the cathode, it is guaranteed sufficient pressing force exists on the cathode, and the situation that the cathode becomes less crowded because of thermal expansion is prevented; and a porous structure is adopted for the head portion of the cathode, a larger current emitting area is achieved, and the current emitting capacity is improved.

Description

technical field [0001] The invention belongs to the field of electric propulsion, and is an electric thruster; specifically, it is a magnetic plasma thruster with a conical porous hollow cathode. Background technique [0002] The magnetoplasma power thruster is a kind of electric thruster, which belongs to the electromagnetic acceleration type according to the acceleration mechanism. Its advantages are high specific impulse, large thrust, and easy realization of high power. However, the working principle of the magnetoplasma thruster is more complicated than that of other electric thrusters, and the design is more difficult. [0003] A core component of a magnetoplasmadynamic thruster is the cathode, whose main function is to emit electrons, ionize the propellant, and generate plasma. Therefore, the current emission capability of the cathode is an important indicator to measure its performance. The common material for the cathode of a magnetoplasma thruster is high-tempera...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F03H1/00
CPCF03H1/0081
Inventor 汤海滨王宝军杨文将李泽峰陈志远
Owner BEIHANG UNIV
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