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Earth static rail communication satellite prototype sample star electric propulsion system

A technology of geostationary orbit and communication satellite, which is applied in the direction of measuring electricity, measuring electrical variables, measuring devices, etc., and can solve the problems such as the complexity of the East Three B electric propulsion system

Active Publication Date: 2015-05-27
CHINA ACADEMY OF SPACE TECHNOLOGY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Dongsan B electric propulsion system is more complex

Method used

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  • Earth static rail communication satellite prototype sample star electric propulsion system
  • Earth static rail communication satellite prototype sample star electric propulsion system
  • Earth static rail communication satellite prototype sample star electric propulsion system

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Experimental program
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Embodiment Construction

[0017] The present invention will be further introduced below in conjunction with the accompanying drawings.

[0018] The complete electric propulsion system configuration and electrical performance interface relationship of Dongsan B platform satellite are as follows: figure 1 . The electric propulsion subsystem mainly includes 4 ion thrusters, storage and supply subsystem (including 2 xenon cylinders + 1 set of pressure regulation module + 4 sets of flow regulation module), power processing unit (PPU), two vector regulation mechanisms and electric Propel control unit. The 100V bus provides input power to the electric propulsion control unit and power processing unit (PPU) in the actuator drive unit (ADU); the electric propulsion control unit supplies power to the solenoid valve and flow controller of the storage and supply subsystem, and controls the storage and supply subsystem The supply and flow adjustment of the gas circuit, and the PPU related control commands are giv...

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Abstract

The invention discloses an earth static rail communication satellite prototype sample star electric propulsion system comprising an electric star electric propulsion system and a structural star electric propulsion system. The electric star electric propulsion system comprises an ion thruster unit S1, an ion thruster unit S2, an ion thruster vector regulating mechanism S, a pressure regulating module, a flow control module N1, a flow control module N2, a flow control module S1, a flow control module S2, an electric propulsion power supply processing unit 1, an electric propulsion power supply processing unit 2, a pipeline and a cable. The earth static rail communication satellite prototype sample star electric propulsion system disclosed by the invention can be used for realizing function check through a relatively simple prototype sample electric propulsion system; the configuration and technical state of the prototype sample star electric propulsion system are determined according to check requirements of electric propulsion performance, and a scheme which is simplified as much as possible is utilized on the premise of sufficiently carrying out test program check; the prototype sample star electric propulsion system can finish the function check of all communication satellite electric propelling systems, besides an ignition function of the thruster; and the ignition function of the thruster needs to be carried out in vacuum, and the whole star test does not have a test state.

Description

technical field [0001] The invention relates to a prototype satellite electric propulsion system of a geostationary orbit communication satellite. Background technique [0002] The development of the initial sample of the satellite includes the development of the electrical star and the structure star. The purpose of developing the initial sample satellite is to verify the correctness of the satellite design scheme, and to solve the exposed design problems. [0003] Electric propulsion technology is an advanced spacecraft propulsion technology that uses electric energy to accelerate the propellant to achieve high specific impulse. Under the same propellant quality, the total impulse output of electric propulsion is several times or even dozens of times that of conventional chemical propulsion systems. . The high specific impulse advantage of electric propulsion can reduce the quality of the satellite platform, increase the lifespan, and increase the payload capacity. On t...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01M15/00G01R31/00
Inventor 李烽王敏潘屹温正刘坤
Owner CHINA ACADEMY OF SPACE TECHNOLOGY