Simple carrier rocket launching system

A carrier rocket and launch system technology, applied in the field of simple launch systems, achieves the effects of simple structure, high safety and reliability, and good processing technology

Active Publication Date: 2014-07-30
GUIZHOU AEROSPACE TIANMA ELECTRICAL TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, there is no precedent for the application of the simple test and launch mode in the launch vehicle in China, so it is necessary to have a system that can be erected as a whole, easy to l

Method used

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Embodiment Construction

[0020] The preferred embodiments of the present invention will be described in detail below in conjunction with the accompanying drawings, so that the advantages and features of the present invention can be more easily understood by those skilled in the art, so as to define the protection scope of the present invention more clearly.

[0021] refer to Figure 1-2 As shown, the simple launch system for launch vehicle testing of the present invention includes a plurality of adapter plates 1 fixedly connected to the ground, and a plurality of adapter plates 1 are sequentially installed with leveling legs 2 and Reducer 3, and the reducer 3 is fixedly connected with the lower surface of the platform body 4, the upper surface of the platform body 4 is equipped with an operating platform 5, and a plurality of supporting devices 6 are evenly distributed on the circumferential direction of the operating platform 5, and the supporting devices 6 are used It is used to support the launch v...

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Abstract

The invention discloses a simple launching system for measuring and launching a carrier rocket. The simple carrier rocket launching system comprises multiple adapter plates fixedly connected with the ground; levelling support legs and a speed reducer are sequentially arranged on the multiple adapter plates from bottom to top; the speed reducer is fixedly connected with the lower surface of a table body; an operation platform is arranged on the upper surface of the table body; multiple support devices are uniformly distributed on the circumferential direction of the operation platform; the support devices are used for supporting the carrier rocket; the simple launching system also comprises an electrohydraulic control system for controlling the speed reducer to act so as to drive the levelling legs for levelling. The simple carrier rocket launching system is simple in structure and good in machining manufacturability; when being overturned, erected and vertically positioned on a launcher, the rocket can be secondly finely tuned by the levelling support legs; the use is convenient, the measuring and launching process of the carrier rocket is simplified, and the response and adaptivity capacities of the launching task are improved; the simple carrier rocket launching system can be used in a site with easy facilities for performing a simple, fast and automatic measuring and launching task; the simple carrier rocket launching system has a function of being used repeatedly for multiple times, and has the advantages of high safety and reliability and the like.

Description

technical field [0001] The invention relates to the technical field of launch vehicles, in particular to a simple launch system for test launch of launch vehicles. Background technique [0002] The launch vehicle can improve the response speed and adaptability of the launch task by simplifying the test and launch process of the launch vehicle. Simple, fast and automated testing tasks can be carried out in a site with simple facilities. However, there is no precedent for the application of the simple test and launch mode in the launch vehicle in China, so it is necessary to have a system that can be erected as a whole, easy to launch, and has the ability to adapt to the launch of a fixed tower and rely on simple facilities, and can achieve rapid launch and requirements. Simple launch system for reusable launch vehicles. Contents of the invention [0003] The present invention mainly solves the technical problems existing in the prior art, thereby providing a simple launch...

Claims

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Application Information

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IPC IPC(8): F41F3/04
Inventor 梁力田洪军阮国民尹兵沈超徐耀钟
Owner GUIZHOU AEROSPACE TIANMA ELECTRICAL TECH
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