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Launching catapult launching system and booster launching method thereof

A launch system and launch vehicle technology, applied in the direction of rocket launchers, weapon types, offensive equipment, etc., can solve the problems of polluting the atmospheric environment, consuming a considerable amount of fuel, and the limited amount of fuel contained in the rocket, so as to avoid pollution and reduce The effect of self-energy consumption

Inactive Publication Date: 2017-06-20
STATE GRID OF CHINA TECH COLLEGE +3
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] At present, the launch of rockets is generally ground launch. The rocket is fixed vertically by the launcher of the rocket, and then when it is launched, the launcher is released, the rocket is ignited, and the booster of the rocket sprays a large amount of flames to make the rocket take off and accelerate. Ascend until it breaks through gravity and enters space, but the amount of fuel that the rocket can hold is limited. When taking off, because it needs to boost the heavy rocket to overcome the acceleration of gravity, it will consume a considerable amount of fuel, making the rocket enter space. After being in space, the supply of fuel to provide power is limited. At the same time, when launching on the ground, a large amount of energy in the burning rocket will pollute the atmospheric environment

Method used

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  • Launching catapult launching system and booster launching method thereof
  • Launching catapult launching system and booster launching method thereof
  • Launching catapult launching system and booster launching method thereof

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Embodiment 1

[0029] Embodiment 1: as figure 1 , figure 2 , image 3 and Figure 4 As shown, the launcher launching system of the present invention includes horizontal rails 3, arc-shaped rails 10 and vertical rails 8 connected in sequence; On the arc track 10 and the vertical track 8;

[0030] The horizontal track 3, the arc track 10 and the vertical track 8 are "work" type rails 23, and the center of the top surface of the "work" type rail 23 is provided with a track groove 22, and the drag hook 19 at the bottom of the open-loop driving device 17 moves on the track Inside slot 22,

[0031] The horizontal track 3 is provided with a steam ejection mechanism 27 for accelerating the trolley 1. The steam ejection mechanism 27 is installed below the horizontal track 3, and a mobile slot for the power output end of the steam ejection mechanism 27 is reserved in the horizontal track 3. The mobile slot It communicates with the track groove 22, and the power output end of the steam ejection m...

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Abstract

The invention provides a launcher launch system and a booster launch method thereof, which belong to the field of booster devices and include horizontal tracks, arc tracks and vertical tracks connected in sequence; Orbit, arc orbit and vertical orbit; it can make the rocket launch use ground resources to obtain the initial velocity, can reduce its own energy consumption, and can reduce the pollution of the rocket jet to the ground environment.

Description

technical field [0001] The invention provides an airlift launching system and a boosting launching method thereof, which belong to the field of boosting devices. Background technique [0002] At present, the launch of rockets is generally ground launch. The rocket is fixed vertically by the launcher of the rocket, and then when it is launched, the launcher is released, the rocket is ignited, and the booster of the rocket sprays a large amount of flames to make the rocket take off and accelerate. Ascend until it breaks through gravity and enters space, but the amount of fuel that the rocket can hold is limited. When taking off, because it needs to boost the heavy rocket to overcome the acceleration of gravity, it will consume a considerable amount of fuel, making the rocket enter space. After being in space, the supply of fuel to provide power is limited. At the same time, when launching on the ground, a large amount of energy in the burning rocket will pollute the atmospheri...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F41F3/04
CPCF41F3/0406
Inventor 牛文东张远镇张传坤王文波刘岱雯赵舒铭胡春静路玲吴志强赵守莉朱国进杨跃宇张丽云
Owner STATE GRID OF CHINA TECH COLLEGE
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