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Rocket transfer erection system

A technology for rockets and erecting arms, which is applied to rocket launchers, transport objects, and object transport vehicles, etc. It can solve problems such as high maintenance costs and long infrastructure construction cycles, reduce the difficulty of docking and adjustment, shorten launch time, Improve the effect of launch

Active Publication Date: 2021-03-02
BEIJING LANDSPACETECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0002] With the development of aerospace technology, especially the vigorous rise of commercial aerospace in recent years, the traditional "three vertical" launch mode has gradually revealed its shortcomings of long infrastructure construction period and high maintenance cost due to the need for a fixed launch tower. Therefore, a fast, flexible, and low-cost launch mode is needed to meet the launch requirements of commercial spaceflight at the present stage

Method used

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Embodiment Construction

[0077] In order to make the purposes, technical solutions and advantages of the embodiments of the present application more clearly understood, the following will clearly illustrate the spirit of the contents disclosed in the present application with the accompanying drawings and detailed descriptions. , when it can be changed and modified by the technology taught by the content of this application, it does not depart from the spirit and scope of the content of this application.

[0078] The illustrative embodiments and descriptions of the present application are used to explain the present application, but are not intended to limit the present application. In addition, elements / members with the same or similar reference numerals used in the drawings and the embodiments are intended to represent the same or similar parts.

[0079] The "first", "second", . .

[0080] Directional terms used herein, such as: up, down, left, right, front or back, etc., are only referring to the ...

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Abstract

The application provides a rocket transfer erection system, which includes a vertical arm, a self-propelled hydraulic axis vehicle and a launch platform; the vertical arm is arranged on the self-propelled hydraulic axis vehicle, and the supported rocket is arranged along the length direction of the vertical arm On the top of the above-mentioned vertical arm; the self-propelled hydraulic axis vehicle is used to transport the supported rocket to the launch pad through the vertical arm; along the length direction of the vertical arm, the vertical arm is sequentially provided with rocket support and tightening devices, The rocket auxiliary hydraulic support device and the rocket rear fulcrum support adjustment device; the rocket support holding device, the rocket auxiliary hydraulic support device and the rocket rear fulcrum support adjustment device form a three-point support for the rocket. This application can safely and reliably transfer and erect the rocket, and can conveniently adjust the rocket with multiple degrees of freedom during the transfer and docking process, effectively reducing the difficulty of docking and adjustment when the rocket is reloaded; this application can greatly Shorten the launch time of the rocket and significantly improve the launch efficiency.

Description

technical field [0001] The application belongs to the technical field of rocket transfer and erection, and in particular relates to a rocket transfer and erection system. Background technique [0002] With the development of aerospace technology, especially the vigorous rise of commercial aerospace in recent years, the traditional "three vertical" launch mode requires a fixed launch tower, and the shortcomings of its infrastructure construction period and high maintenance cost are gradually revealed. Therefore, a fast, flexible and low-cost launch mode is needed to meet the launch needs of commercial aerospace at this stage. [0003] Most successful commercial aerospace companies abroad adopt the "three-level" test and launch mode, that is, the launch mode of horizontal assembly, horizontal transfer, horizontal testing, and vertical launch. Therefore, it is particularly important to reliably support and carry the rocket body during the process of rocket reloading, transfer ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F41F3/04F41F3/052B60P3/00B60P7/135
CPCF41F3/04F41F3/052B60P3/00B60P7/135
Inventor 张瑜张彦杰吴雪
Owner BEIJING LANDSPACETECH CO LTD
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