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Rocket transfer and 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: 2020-04-17
BEIJING LANDSPACETECH CO LTD
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  • 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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  • Rocket transfer and erection system
  • Rocket transfer and erection system
  • Rocket transfer and erection system

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Embodiment Construction

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

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

[0079] The terms "first", "second", ... etc. used herein do not specifically refer to a sequence or order, nor are they...

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Abstract

The invention provides a rocket transfer and erection system which comprises an erection arm, a self-propelled hydraulic axis vehicle and a launcher. The erection arm is arranged on the self-propelledhydraulic axis vehicle; a rocket to be supported is arranged on the top part of the erection arm along the length direction of the erection arm; the self-propelled hydraulic axis vehicle is used fortransporting the rocket to be supported to the launcher through the erection arm; and along the length direction of the erection arm, a rocket supporting and clamping device, a rocket auxiliary hydraulic supporting device and a rocket rear supporting point supporting and adjusting device are sequentially arranged on the erection arm, and form a three-point support for the rocket. According to therocket transfer and erection system provided by the invention, the rocket can be safely and reliably transferred and erected, the rocket can be conveniently adjusted at multiple degrees of freedom inthe transferring and docking process, and the difficulty in docking and adjusting the rocket during transferring is effectively reduced; and the launching time of the rocket can be greatly shortened,and the launching efficiency is remarkably improved.

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 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 this stage. [0003] Most of the successful foreign commercial aerospace companies adopt the "three-level" test and launch mode, that is, the launch mode of horizontal assembly, horizontal transfer, horizontal test, and vertical launch. Therefore, it is particularly important to reliably support and carry the rocket body in the process of rocket rel...

Claims

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Application Information

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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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