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A high-speed carrier vehicle and method capable of realizing horizontal launch of carrier rockets

A launch vehicle and rocket launch technology, applied in rocket launch devices, offensive equipment, weapon types, etc., can solve problems such as limiting rocket payload, rocket providing initial velocity, and low rocket efficiency, and reducing the number of bundled booster rockets , improve efficiency, simplify the effect of launching procedures

Active Publication Date: 2017-07-11
隋广林
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In these two forms of rocket launch, the initial velocity of the rocket is zero, which makes the efficiency of the rocket extremely low, the waste of fuel is large, and the thrust-to-weight ratio is too small, which limits the payload of the rocket to a large extent.
At the same time, the way of vertical launch is also greatly affected by the weather
[0004] The rocket launcher makes the rocket more maneuverable, but the essence of the launch of the rocket launcher is the vertical or prone rocket launch carried out by the launcher in a static state, so the launcher is only a vehicle for carrying and launching statically. The tool cannot use its own kinetic energy to provide the rocket with a certain initial velocity, so there are still many defects in the vertical or prone position launch mode

Method used

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  • A high-speed carrier vehicle and method capable of realizing horizontal launch of carrier rockets
  • A high-speed carrier vehicle and method capable of realizing horizontal launch of carrier rockets
  • A high-speed carrier vehicle and method capable of realizing horizontal launch of carrier rockets

Examples

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Effect test

Embodiment 1

[0043] Embodiment 1: A kind of high-speed carrier vehicle that can realize the horizontal launch of carrier rocket, its structure is as follows figure 1 Shown: include: car body 3, car body 3 is fixedly connected with rocket launcher 2, and rocket launcher 1 and igniter 7 are installed on rocket launcher 2, and igniter 7 is positioned at the tail of launch vehicle 1; Control system is installed on vehicle Inside body 3;

[0044] The bottom of the car body 3 is fixedly connected with the carrier frame 4, and the wheel 6 is installed on the carrier frame 4;

[0045] The vehicle body 3 is driven by a power unit.

[0046] The rocket launcher 2 is arranged on an incline, and the top is an inclined surface.

[0047] As the choice of the control system, the device can be controlled by man or man, that is, wireless control or program control.

[0048] The carrying frame 4 may be an existing train bogie.

[0049] The power unit is a propeller 9 . The propeller 9 can be selected as...

Embodiment 2

[0053] Embodiment 2: A kind of carrier rocket horizontal launch high-speed power carrying vehicle, its structure is as follows figure 2 Shown: include: car body 3, car body 3 is fixedly connected with rocket launcher 2, rocket launcher 2 is installed with launch vehicle 1 and igniter 7, and igniter 7 is positioned at the tail of launch vehicle 1;

[0054] The bottom of the car body 3 is fixedly connected with the carrier frame 4, and the wheel 6 is installed on the carrier frame 4;

[0055] The vehicle body 3 is driven by a power unit.

[0056] The power device is a high-speed rail motor car 10, and the high-speed rail motor car 10 pulls the car body 3 to move.

[0057] As a better option, a wireless or program control system can be installed on the vehicle body 3 to facilitate the unmanned launch of the launch vehicle 1 .

[0058] The carrying frame 4 may be an existing train bogie.

[0059] In this embodiment, the carrier frame 4 and the wheel 6 can also be replaced with...

Embodiment 3

[0061] Embodiment 3: A kind of carrier rocket horizontal launching high-speed power carrying vehicle, its structure is as follows image 3 Shown: including: a car body 3 with a magnetic levitation structure, the car body 3 is fixedly connected with the rocket launcher 2, and the rocket launcher 2 is installed with a launch vehicle 1 and an igniter 7, and the igniter 7 is located at the tail of the launch vehicle 1;

[0062] The vehicle body 3 is driven by a power unit.

[0063] The rocket launcher 2 is arranged on an incline, and the top is an inclined surface.

[0064] The power unit is a magnetic levitation locomotive 11 . The magnetic levitation vehicle head 11 pulls the vehicle body 3 to move.

[0065] As a better option, a wireless or program control system can be installed on the car body 3 to facilitate the unmanned launch of the launch vehicle 1 .

[0066] The carrying frame 4 may be an existing train bogie.

[0067] The principle of this embodiment is: the magneti...

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Abstract

The invention relates to a high-speed carrier vehicle capable of realizing the horizontal launch of carrier rockets and a method thereof. The high-speed vehicle part mainly includes a car body, a power unit, a control system, a rocket launcher and an igniter; the igniter is installed on the rocket launcher, and the rocket launcher is installed on the vehicle body, and the rocket launcher has an inclined ; The lower part of the car body is fixedly connected with the bearing frame, and wheels are installed on the carrier frame; the car body is driven by a power device. By designing a brand-new structure, the carrier vehicle device realizes the rocket's high-speed movement and prone position launch, so that the rocket has a high initial velocity during launch, thereby improving the efficiency of the rocket, saving a lot of fuel, reducing the rocket's own weight and increasing the thrust-to-weight ratio and load.

Description

technical field [0001] The invention relates to the technical field of rocket launch, in particular to a high-speed carrier vehicle and a method capable of realizing horizontal launch of a carrier rocket. Background technique [0002] Currently common forms of rocket launch include vertical launch and prone launch. [0003] In these two rocket launch forms, the initial velocity of the rocket is zero, which makes the efficiency of the rocket extremely low, the waste of fuel is large, and the thrust-to-weight ratio is too small, which limits the payload of the rocket to a large extent. At the same time, the way of vertical launch is also greatly affected by the weather. [0004] The rocket launcher makes the rocket more maneuverable, but the essence of the launch of the rocket launcher is the vertical or prone rocket launch carried out by the launcher in a static state, so the launcher is only a vehicle for carrying and launching statically. However, the tool cannot use its ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F41F3/04
Inventor 隋广林
Owner 隋广林
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