Iodine medium ground gas supply device for Hall thruster and using method

A technology of Hall thruster and air supply device, which is applied in the direction of thrust reverser, measuring device, instrument, etc. It can solve the problems of difficult flow control and severe influence of flow change, and achieve good performance of thrust parameters, prevention of condensation, atomic high quality effect

Active Publication Date: 2020-05-12
LANZHOU INST OF PHYSICS CHINESE ACADEMY OF SPACE TECH
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

The temperature change has a severe impact on the flow change, and the flow control is difficult

Method used

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  • Iodine medium ground gas supply device for Hall thruster and using method
  • Iodine medium ground gas supply device for Hall thruster and using method
  • Iodine medium ground gas supply device for Hall thruster and using method

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Embodiment Construction

[0022] In order to enable those skilled in the art to better understand the solution of the present application, the technical solution in the embodiment of the application will be clearly and completely described below in conjunction with the accompanying drawings in the embodiment of the application. Obviously, the described embodiment is only It is an embodiment of a part of the application, but not all of the embodiments. Based on the embodiments in this application, all other embodiments obtained by persons of ordinary skill in the art without creative efforts shall fall within the scope of protection of this application.

[0023] It should be noted that the terms "first" and "second" in the description and claims of the present application and the above drawings are used to distinguish similar objects, but not necessarily used to describe a specific sequence or sequence. It should be understood that the data so used may be interchanged under appropriate circumstances for...

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Abstract

The invention relates to the technical field of aerospace Hall electric propulsion, in particular to an iodine medium ground gas supply device for a Hall thruster and a using method. The iodine mediumground gas supply device includes an iodine vapor generating unit and an iodine vapor flow control unit, wherein the iodine vapor generating unit includes a solid iodine storage tank and a first pressure sensor. The iodine vapor flow control unit includes a shut-off valve, a pressure relief valve, a second pressure sensor and a flow control valve. The iodine medium ground gas supply device for the Hall thruster adopts an iodine medium propellant to achieve good thrust parameter performance, and the thruster is more efficient. An iodine medium is heated and sublimated into iodine vapor for transportation, the condensation of the iodine vapor in the transportation process is prevented, the flow rate of the iodine vapor can be controlled in real time, and it is ensured that the iodine vaporcan be stably and accurately transported to the Hall thruster.

Description

technical field [0001] The application relates to the technical field of aerospace Hall electric propulsion, in particular to an iodine medium ground gas supply device for a Hall thruster and a method for using it. Background technique [0002] With the development of aerospace technology and the continuous maturity of electric propulsion technology, more and more electric thrusters are being developed and developed by the aerospace industry of various countries. Compared with traditional chemical thrusters, electric thrusters have the characteristics of high specific impulse, long life, compact structure, and small size, and have significant application prospects in satellite attitude control, orbit correction, orbit maintenance, and power compensation. [0003] Among many electric thrusters, the Hall thruster has attracted widespread attention because of its simple structure, easy operation, and high utilization of working fluid. The mainstream Hall thruster propellant is...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F03H1/00G01D21/02
CPCF03H1/0012G01D21/02
Inventor 顾森东马天驹王祥龙程彬徐涛李玉峰张雪儿姜玉恒祁杰张永红
Owner LANZHOU INST OF PHYSICS CHINESE ACADEMY OF SPACE TECH
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