CN101566449A

CN101566449A - Gun-boosted missile

Info

Publication number: CN101566449A
Application number: CNA2008101628351A
Authority: CN
Inventors: 寿国伟
Original assignee: Individual
Current assignee: Individual
Priority date: 2008-12-03
Filing date: 2008-12-03
Publication date: 2009-10-28

Abstract

The invention relates to a gun-boosted missile, in particular to a missile capable of being launched in a gun barrel. The missile is characterized by comprising an artillery and a missile, wherein a tail part of the missile is made to be the same as that of a shell for adapting to launch by the artillery. During use, the missile is first launched by the artillery and then propelled by a thruster to continue to fly forward. The gun-boosted missile solves the problem that the prior missile and shell assume a normal speed by gradually accelerating from stillness and decelerate immediately when coming out from the gun barrel, and improves the initial speed of the missile. The missile can keep normal flight after being launched, and the flight stability and fighting performance of the missile are ensured.

Description

Gun launched missile

Technical field

The present invention is a kind of guided missile that can launch in bore, missile tail is made identical with the shell afterbody, utilizes cannon that guided missile is launched away, to improve the initial velocity of missile flight.

Technical background

As everyone knows, shell is two kinds of different weapons with guided missile, shell is to launch by cannon, utilize the expanding gas that gun propellant combustion produces in the shell that bullet is released bore during emission, utilize the coherence of bullet to fly to target, heading determined by the sensing of gun tube, and the maximum speed of flying speed when going out thorax is slack-off gradually, hits the mark at last or falls earthward and finish shooting course.Guided missile is to be promoted by rocket propulsion, guided missile speed under rocket propulsion promotes accelerates gradually during emission, continue flight forward under rocket propulsion promotes after reaching certain speed, heading can be controlled with multiple aiming means such as infrared guidance and radar guidances, until missile-target impact.Though the form that rocket gun and recoilless gun have shell and guided missile to combine, the flight course of its body is basic similar to guided missile.

In sum, present guided missile and shell go out the flying speed behind the thorax, are not that to begin to quicken to reach normal speed gradually be exactly to begin to slow down gradually once going out thorax from static.Therefore, people expect to occur a kind of once going out the guided missile that thorax can keep normal flight speed, to improve the combat performance of guided missile.

Summary of the invention

The present invention is a kind of guided missile that can launch in bore, missile tail is made identical with the shell afterbody, utilizes cannon that guided missile is launched away, makes guided missile can keep normal flight speed once going out thorax, with the flight stability that improves guided missile and the combat performance of guided missile.

Gun launched missile of the present invention is characterized in that: it comprises one piece of guided missile, missile tail is made identical with the shell afterbody, to adapt to cannon emission.Earlier with cannon guided missile is launched out thorax during use, flight forward under rocket propulsion promotes again is until missile-target impact.

Beneficial effect of the present invention: gun launched missile of the present invention is with cannon guided missile to be launched away earlier, makes guided missile can keep normal flight speed once going out thorax, flight forward under rocket propulsion promotes again.Can improve the flight stability of guided missile and the combat performance of guided missile.

Description of drawings

Do not have

The specific embodiment

Gun launched missile of the present invention is that the emission cannon is done corresponding improvement, missile tail is made identical with the shell afterbody, to adapt to cannon emission.With cannon guided missile is launched away earlier flight forward under rocket propulsion promotes again during use.After going out, MISSILE LAUNCHING select suitable guided missile guidance mode to make guided missile fly to target.

Claims

1, a kind of gun launched missile.It is characterized in that: it comprises a cannon and one piece of guided missile, with cannon guided missile is launched away earlier during use, makes guided missile continue flight forward again under rocket propulsion promotes.Solving present guided missile and shell, to go out flying speed behind the thorax be not that to begin to quicken to reach gradually normal speed be exactly once going out the problem that the thorax beginning is slowed down gradually, improving the initial velocity of guided missile from static.Can remain normal flight after making MISSILE LAUNCHING, guarantee the stability and the combat performance of missile flight.

2, gun launched missile according to claim 1 is characterized in that: said guided missile is a kind of bullet shells.Missile tail is made identical with the shell afterbody, integral body is one piece of shell, available cannon emission.