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A multi-satellite parallel launch device based on auxiliary support

A technology for auxiliary support and launching devices, which is applied in launching systems, transportation and packaging, and space navigation equipment, etc. It can solve the problems of low space utilization of satellite fairings and occupying the payload of launch vehicles, etc., to improve performance and adaptability , improve load launching capability, simple structure

Active Publication Date: 2022-07-01
SHANGHAI AEROSPACE SYST ENG INST
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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

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  • A multi-satellite parallel launch device based on auxiliary support
  • A multi-satellite parallel launch device based on auxiliary support
  • A multi-satellite parallel launch device based on auxiliary support

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Embodiment Construction

[0027] The following will combine Figure 1 to Figure 5 A multi-satellite parallel launch 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 the detailed implementation mode and specific operation process are given. The protection scope of the invention is not limited to the following embodiments, and those skilled in the art can modify and modify the invention 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 launch 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, the beam system is installed The platform 3 is set at the top of the support cabin body 1, the support rod system ...

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Abstract

The invention relates to a multi-satellite parallel launch device based on auxiliary support, comprising a support cabin body, a support rod system, a beam system installation platform and at least two installation parts for installing satellites to be launched. At the top of the support cabin, the support rod is located in the support cabin, and is supported between the support cabin and the beam system installation platform, and the installation portion is installed in the support cabin The cabin and beams are installed on the platform. The invention adopts the method of multi-satellite parallel layout based on auxiliary struts, overcomes the shortcomings of the multi-satellite series layout occupying the payload weight and increasing the height of the satellite fairing, and solves the problem that the multi-satellite series launch takes up the payload of the launch vehicle and the satellite fairing. Insufficient space utilization. The invention has a simple structure, reduces the structural weight of the multi-satellite parallel launch device, improves the structural efficiency, improves the performance and adaptability of the multi-satellite launch device, and improves the launch capability of the carrier rocket.

Description

technical field [0001] The invention relates to the technical field of launch vehicles, in particular to a multi-satellite parallel launch device based on auxiliary support. Background technique [0002] One rocket multi-satellite launch technology refers to the technology of using one rocket to launch multiple satellites into predetermined orbits at one time. This technology can shorten the launch cycle of a single satellite and reduce the launch cost, which is an important way to reduce the launch cost of launch vehicles. [0003] At present, in order to achieve the launch of multiple satellites with one rocket, a dedicated carrying cabin needs to be developed to realize its layout. Previous models often used a multi-satellite tandem layout, that is, adding transition cabins and support cabins to achieve its layout, and then installing satellites through adapters. This method occupies the payload weight of the rocket and reduces the carrying capacity of the rocket. The t...

Claims

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Application Information

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Patent Type & Authority Patents(China)
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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