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Space application communication platform based on rail retaining last stage of carrier rocket

A communication platform and launch vehicle technology, applied in radio transmission systems, electrical components, transmission systems, etc., can solve problems such as falling into the atmosphere and burning, ground buildings, human and livestock hazards, etc., to achieve low transformation costs, effective output and The effect of high investment ratio and high maturity

Active Publication Date: 2017-02-01
BEIJING INST OF ASTRONAUTICAL SYST ENG +1
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  • Summary
  • Abstract
  • Description
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AI Technical Summary

Problems solved by technology

[0002] At present, after the completion of the mission of the launch vehicle to launch the satellite, the final stage of the launch vehicle and the satellite adapter stay in space together and become space junk, which is completely out of control and falls into the atmosphere after a period of time and burns; if it cannot be completely burned, it will also damage the buildings on the ground , human and livestock hazards

Method used

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  • Space application communication platform based on rail retaining last stage of carrier rocket
  • Space application communication platform based on rail retaining last stage of carrier rocket
  • Space application communication platform based on rail retaining last stage of carrier rocket

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Embodiment Construction

[0041] Below in conjunction with accompanying drawing and specific embodiment the present invention is described in further detail:

[0042] Such as figure 1Shown is a schematic layout diagram of the aerospace application communication platform of the present invention. It can be seen from the figure that the aerospace application communication platform of the present invention is based on the last stage of the carrier rocket, including a satellite adapter 2, an instrument mounting plate 8, an attitude control system sensor, an actuator, and an attitude control system. Control tank 7, battery 11, power control unit (PCU) 12, task manager 4, communication relay load and solar panels 1, 2, wherein the communication relay load includes antenna 14 and information processing equipment 15, and the actuator includes The reaction flywheel 5, the magnetic torque device 13 and the attitude control nozzle 16, wherein the satellite adapter 2 is a hollow circular platform structure with bo...

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Abstract

The invention relates to a space application communication platform based on a rail retaining last stage of a carrier rocket. The space application communication platform comprises a satellite adapter, an instrument mounting plate, an attitude control system sensor, an actuator, a storage battery, a power control unit, a task manager, a communication relay load and a solar panel, wherein the communication relay load comprises an antenna and an information processing device, the actuator comprises a counterforce flywheel, a magnetic torque and an attitude control exhaust pipe, the satellite adapter is of a hollow circular truncated cone structure with two open ends, and the instrument mounting plate is mounted at a bottom end of the circular truncated cone structure. According to the communication platform provided by the invention, the surplus carrying capacity of the carrier rocket is fully excavated, any necessary devices necessary for realizing an expansion task are deployed in the structural cabin segment of the satellite adapter by the ideas of loading and restructuring, the communication relay load is loaded, high-rail, middle-rail and low-rail space cloud communication service systems for commercial aerospace are constructed to realize measurement and control, communication and other directional services without secondary launching costs, thereby having the advantages of low-cost operation.

Description

technical field [0001] The invention relates to an aerospace application communication platform based on the last stage of a carrier rocket remaining in orbit, and belongs to the technical field of military-civilian integration. Background technique [0002] At present, after the completion of the mission of the launch vehicle to launch the satellite, the final stage of the launch vehicle and the satellite adapter stay in space together and become space junk, which is completely out of control and falls into the atmosphere after a period of time and burns; if it cannot be completely burned, it will also damage the buildings on the ground , humans and livestock. Contents of the invention [0003] The purpose of the present invention is to overcome the above-mentioned defects of the prior art, and provide a communication platform for aerospace applications based on the final stage of the carrier rocket. The equipment required for the extended mission is arranged in the adap...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H04B7/185
CPCH04B7/18515H04B7/18519
Inventor 王国辉安雪岩陆浩然刘靖东于秀丽王传魁荣晶晶彭越王岩夏伟强
Owner BEIJING INST OF ASTRONAUTICAL SYST ENG
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