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Multi-satellite parallel launching device based on auxiliary supporting

A technology of auxiliary support and launch device, applied in launch systems, transportation and packaging, space navigation equipment, etc., can solve the problems of low utilization of satellite fairing space, occupying the payload of launch vehicles, etc., to improve performance and adaptability , Improve the load launch ability, the effect of simple structure

Active Publication Date: 2020-12-11
SHANGHAI AEROSPACE SYST ENG INST
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to provide a multi-satellite parallel launching device based on auxiliary support to solve the technical problems in the prior art that the multi-satellite series launch occupies the payload of the launch vehicle and the space utilization rate of the satellite fairing is low

Method used

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  • Multi-satellite parallel launching device based on auxiliary supporting
  • Multi-satellite parallel launching device based on auxiliary supporting
  • Multi-satellite parallel launching device based on auxiliary supporting

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Embodiment Construction

[0027] The following will combine Figure 1 to Figure 5 A multi-satellite parallel launching device based on auxiliary support provided by the present invention is described in detail. This embodiment is implemented on the premise of the technical solution of the present invention, and a detailed implementation method and specific operation process are given. However, this The protection scope of the invention is not limited to the following embodiments, and those skilled in the art can modify and embellish it within the scope of not changing the spirit and content of the invention.

[0028] Please refer to Figure 1 to Figure 5 , a multi-satellite parallel launching device based on auxiliary support, comprising a support cabin body 1, a support rod system 2, a beam system installation platform 3 and at least two installation parts 4 for installing satellites to be launched, and the beam system is installed The platform 3 is arranged on the top of the support cabin body 1, th...

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Abstract

The invention relates to a multi-satellite parallel launching device based on auxiliary supporting. The multi-satellite parallel launching device based on the auxiliary support comprises a supportingcabin body, a supporting rod system, a beam system mounting platform and at least two mounting parts for mounting satellites to be launched, the beam system mounting platform is arranged at the top end of the supporting cabin body, the supporting rod system is positioned in the supporting cabin body and is arranged between the supporting cabin body and the beam system mounting platform in a supporting mode, and the mounting parts are mounted on the supporting cabin body and the beam system mounting platform. A multi-satellite parallel layout mode based on auxiliary supporting rods is adopted,the defects that a multi-satellite series layout occupies the effective load weight and increases the height of a satellite fairing are overcome, and the defects that multi-satellite series launchingoccupies the effective load of a carrier rocket and the space utilization rate of the satellite fairing is low are overcome. The multi-satellite parallel launching device based on the auxiliary support is simple in structure, the structural weight of the multi-satellite parallel launching device is reduced, the structural efficiency is improved, the performance and adaptability of the multi-satellite launching device are improved, and the load launching capacity of the carrier rocket is improved.

Description

technical field [0001] The invention relates to the technical field of launch vehicles, in particular to a multi-satellite parallel launching device based on auxiliary supports. Background technique [0002] The multi-satellite launch technology with one rocket refers to the technology of launching multiple satellites into predetermined orbits with one rocket at a time. This technology can shorten the launch period of a single satellite and reduce the launch cost, which is an important way to reduce the launch cost of the launch vehicle. [0003] At present, in order to realize the multi-satellite launch of a launch vehicle, it is necessary to develop a special carrying cabin to realize its layout. Previous models often used a multi-satellite series layout, that is, adding a transition cabin and a support cabin to realize its layout, and then installing satellites through adapters. This method takes up the payload weight of the rocket and reduces the carrying capacity of t...

Claims

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Application Information

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IPC IPC(8): B64G1/00
CPCB64G1/002
Inventor 赵学成秦震陈佳刘涛杨颜志
Owner SHANGHAI AEROSPACE SYST ENG INST
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