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Rocket weapon or emitter launching system and method

A rocket weapon and launch system technology, applied in the field of box-type rocket launch devices, can solve the problems of long development cycle of rocket launch vehicles, affecting model project approval or contract bidding, and short development cycle, so as to broaden the types of launch modes and shorten the development cycle. , the effect of strong environmental adaptability

Active Publication Date: 2019-05-17
湖北航天飞行器研究所
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] However, in recent years, rocket weapon systems are faced with increasingly urgent requirements for low funding, short cycle time, and high reliability in the development process. Therefore, some types of weapon systems will have a long development cycle for rocket launchers or insufficient funds in the initial stage of development. Timely output cannot be guaranteed due to various reasons, which will affect the flight test launch mission of the box rocket, which in turn will affect the model project approval or contract bidding
[0004] Therefore, the traditional box-type rocket launch vehicle cannot meet the requirements of low R&D and production costs, short R&D period and high reliability in reality.

Method used

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  • Rocket weapon or emitter launching system and method
  • Rocket weapon or emitter launching system and method
  • Rocket weapon or emitter launching system and method

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0053] like figure 1 Shown, rocket weapon or launcher launch system, including:

[0054] The base platform 1 is fixed on the ground when in use.

[0055] Erecting platform 2, one end is rotatably fixed on the fixed position of base platform;

[0056] Oblique supporting platform 3, one end is rotatably connected with the erecting platform, and the other end is a free end,

[0057] Wherein, a locking structure is provided at a position away from the fixed position of the base platform,

[0058] When the erecting platform is erected and rotated to a predetermined angle, the free end of the inclined support platform is fixed and locked on the base platform through the locking structure arranged on the base platform.

Embodiment 2

[0060] On the basis of Embodiment 1, as an optimization, one end of the erecting platform is fixed on the fixed position of the base platform by a fixed pin; and / or,

[0061] One end of the inclined support platform is rotatably connected with the erecting platform through a pin shaft;

[0062] and / or,

[0063] The locking structure is a pin hole arranged on the base platform,

[0064] When fixing, the fixed pin shaft passes through the pin shaft hole, and the free end of the inclined support platform is connected and fixed at the pin shaft hole through the fixed pin shaft 6 .

[0065] By using the solution of the fixed pin shaft, the structure is simple, the design is convenient for rapid design, and the design and manufacturing time is shortened.

Embodiment 3

[0067] On the basis of the above-mentioned embodiment 1-2, the free end of the oblique support platform is provided with a double-ended screw, and the hole on the oblique support platform can be aligned with the pin shaft hole through the double-ended screw for installation of the fixed pin shaft.

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Abstract

The invention discloses a rocket weapon or emitter launching system. The rocket weapon or emitter launching system is characterized by comprising a base platform which is fixedly arranged on the ground during use, a rising vertical platform which one end of the rising vertical platform is rotatably fixed at a fixed position of the base platform, an inclined supporting platform which one end of theinclined supporting platform is connected with the rising vertical platform in a rotatable mode and the other end of the inclined supporting platform is a free end, wherein a locking structure is arranged at the position, away from the fixed position, of the base platform, when the rising vertical platform is vertically rotated to a preset angle, the free end of the inclined supporting platform is fixedly locked on the base platform through the locking structure arranged on the base platform. According to the system and the method, a pure mechanical structure scheme is adopted to complete thedesign of a box type rocket launching device, the problems of emission tasks under the conditions of low cost, fast rhythm and high reliability are solved, and the system and the method have the characteristics of easiness in operation, low in cost, high in strength, and the emission mode types of the box type rocket is widened.

Description

technical field [0001] The invention belongs to rocket launching technology, and specifically designs a box-type rocket launching device. Background technique [0002] The launch methods used for reverse thrust jet launchers such as box-type rockets or missiles mostly use the launch method of rocket launch vehicles. At the same time, the rocket launch vehicle has the outstanding advantages of high automation and high launch accuracy, so the box-type rocket launch vehicle is a conventional equipment that must be designed during the rocket development process. [0003] However, in recent years, rocket weapon systems are faced with increasingly urgent requirements for less funding, shorter cycle times, and higher reliability during the development process. Therefore, some types of weapon systems will suffer from the long development cycle of rocket launchers or insufficient funds in the initial stage of development. Timely output cannot be guaranteed due to various reasons, wh...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F41F3/04
Inventor 李盛薛士明蔺法鹏刘斌谢永刚
Owner 湖北航天飞行器研究所
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