Ground launching system and launching method for medium-sized liquid carrier rocket

A technology for launch vehicles and launch systems, which is applied in rocket launch devices, weapon types, offensive equipment, etc., can solve problems such as limited launch of fixed launch stations, excavation of diversion grooves, etc., and achieves low development difficulty and reduced launch costs. , the effect of increasing launch flexibility

Pending Publication Date: 2022-05-10
北京天兵科技有限公司
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] In order to solve the problem that traditional liquid rocket launches are limited to fixed launch stations and diversion grooves need to be excavated, the invention provides a ground launch system and launch method for medium-sized liquid rockets. The ground launch system consists of a launch frame, a launch platform, a guide Composed of streamers, it can be moved at different launching stations, increasing the flexibility of launching

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  • Ground launching system and launching method for medium-sized liquid carrier rocket
  • Ground launching system and launching method for medium-sized liquid carrier rocket
  • Ground launching system and launching method for medium-sized liquid carrier rocket

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Embodiment Construction

[0046] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in combination with specific embodiments and with reference to the accompanying drawings. It should be understood that these descriptions are exemplary only, and are not intended to limit the scope of the present invention. Also, in the following description, descriptions of well-known structures and techniques are omitted to avoid unnecessarily obscuring the concept of the present invention.

[0047] Medium Liquid Launch Vehicle Ground Launch System, combined with figure 1 , including: launch frame 1, launch pad 2 and deflector 3.

[0048] (1) launcher

[0049]The launching frame 1 includes a truss foundation 12 , an erecting arm 11 , and an erecting oil cylinder 13 . The truss foundation 12 is placed on the launch site pad, has no mechanical connection with the launch site pad, and is not limited to a speci...

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Abstract

The invention relates to a medium-sized liquid carrier rocket ground launching system and launching method. The launching system comprises a launching rack, a launching pad and a fluid director. The launching rack comprises a truss foundation and an erecting arm, the truss foundation is placed on a launching site, and the erecting arm bears the carrier rocket which is horizontally placed when being horizontally placed and can drive the carrier rocket to erect; the launching pad is fixed to a truss foundation and used for bearing the carrier rocket; the fluid director is fixed to the truss foundation, located between the launching pad and the truss foundation and used for exhausting and guiding tail flames of a rocket engine. The launching system can move at different launching stations, so that the launching flexibility is improved. The fluid director is used for discharging and guiding rocket take-off gas flow, and a diversion trench does not need to be built in a launching station. All launching devices only need a flat hardened cement field level and do not depend on a certain specific launching site.

Description

technical field [0001] The invention relates to the technical field of rocket launch systems, in particular to a ground launch system and launch method for a medium-sized liquid carrier rocket. Background technique [0002] There are many ways to launch carrier rockets, such as land-based, sea-based, and air-launched. The launch method of small rockets is flexible, and the launching equipment such as erection and tail flame diversion are relatively simple. Solid launch vehicles are generally small rockets, which are easier to realize vehicle-mounted mobile launches. Medium-sized rockets, with a payload of 5-20 tons, especially medium-sized liquid launch vehicles, need to meet multiple guarantee conditions, and the launch equipment is relatively complicated. The rocket is erected on the launch pad. When the rocket is ignited and takes off, the high-temperature and high-speed gas flow from the engine needs to be smoothly guided to prevent the rocket and other equipment on th...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F41F3/04
CPCF41F3/04
Inventor 李永俊吴雪韩召洋田伟枫赵立涛刘兴隆孙目朱正辉李晓昕
Owner 北京天兵科技有限公司
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