Powered teaching rocket launcher

A launcher and rocket technology, which is applied to rocket launchers, offensive equipment, weapon types, etc., can solve problems such as installation hazards, high mass, and high engine cost

Pending Publication Date: 2020-10-30
NAT UNIV OF DEFENSE TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, for the rocket launch process, teaching rockets with built-in engines are more dangerous in the storage, transfer, preservation and launch process, especially the installation process.
Moreover, the cost of the engine is high, usually occupying more than 30% of the entire teaching rocket; the mass is large, accounting for more than 30% of the entire rocket mass, so the engine occupies a large amount of space at the tail of the teaching rocket

Method used

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  • Powered teaching rocket launcher
  • Powered teaching rocket launcher
  • Powered teaching rocket launcher

Examples

Experimental program
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Effect test

Embodiment Construction

[0028] Figure 1 to Figure 8 A specific embodiment of a powered teaching rocket launcher of the present invention is shown, as figure 1 , figure 2 , image 3 , Figure 7 As shown, the launcher base 1 is included, the front and rear ends of the launcher base 1 are respectively equipped with a pitch angle adjustment support rod 11 and a guide rail slide bracket 12, and the guide rail slide table 2 is erected on the pitch angle adjustment support rod 11 and the guide rail slide bracket 12, the guide rail slide 2 is provided with a rocket sliding groove 21 for the rocket to move forward along the central axis, and a launch booster for pushing the rocket forward is installed at the tail end of the guide rail slide 2 3. In this embodiment, the launch angle of the guide rail slide table 3 is adjusted by the pitch angle adjustment support rod 11, the guide rail required for rocket launch is provided by the guide rail slide table 2, and the rocket is boosted to the launch speed re...

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Abstract

The invention discloses a powered teaching rocket launcher. The launcher comprises a launcher base, wherein a pitch angle adjustment support rod and a guide rail sliding table bracket are installed atthe front and rear ends of the launcher base respectively, guide rail sliding table frames are installed on the pitch angle adjustment support rod and the guide rail sliding table bracket, a rocket sliding groove for a rocket to move forwards is formed in the middle axis of a guide rail sliding table, and a launch booster for pushing the rocket forwards is arranged at the tail end of the guide rail sliding table. Compared with a traditional launcher, the launcher provides power required for the teaching rocket to fly through the launch booster, so that the mass of the teaching rocket is reduced by at least 30%, and more built-in instrument and equipment reduce the design cost and difficulty of the rocket. Due to the use of the launch booster, an engine of the rocket is canceled, so that the process of launch, storage and transportation is safer, and the purposes of low-cost required for tests and safe launch of the rocket are achieved relevantly.

Description

technical field [0001] The invention belongs to the field of rocket launch, in particular to a powered teaching rocket launcher. Background technique [0002] The current mainstream rocket launch, especially the teaching rocket launch, mainly uses the built-in rocket engine to provide the power for the rocket to fly forward. A rocket motor is installed at the tail of the rocket body to push the rocket to a preset flight speed to achieve the purpose of boosting the rocket. [0003] Existing launchers are usually unpowered, and only provide a flight glide track with adjustable azimuth and launch angle. After the rocket is placed on the launcher, it is ignited and launched, and it flies forward under the working thrust of the rocket's built-in engine. But for the rocket launch process, teaching rockets with built-in engines are more dangerous in the storage, transfer, preservation and launch process, especially the installation process. Moreover, the cost of the engine is hig...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F41F3/04
CPCF41F3/0406
Inventor 江振宇许秋平白锡斌刘龙斌张士峰
Owner NAT UNIV OF DEFENSE TECH
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