KR101937729B1 - Firing test device and method for missile cable - Google Patents

Abstract

The present invention relates to an explosion test device and a method for verifying a guided missile cable, comprising: a guided missile launch system (10) applying an ignition signal to a guided missile (20); a guided missile cable (40) which is a wiring in the guided missile (20), and which delivers the signal applied from the guided missile launch system (10) to an explosion device (30); and an ignition box (50) which prevents shards from flying towards the outside when the explosion device (30) explodes. According to the present invention, a real guided missile cable can undergo an explosion test in the ignition box without additional connection, thereby verifying reliability of the guided missile cable which is a wire in the guided missile.

Description

TECHNICAL FIELD [0001] The present invention relates to a test apparatus and method for testing a missile cable,

More particularly, the present invention relates to an apparatus and a method for aeronautical test for verifying a missile caravan cable capable of reliably verifying a missile caravan cable.

Guided missiles are bombs or shells that reach the target precisely and expose them to the target by induction of radar or infrared rays. The missile is launched and propelled by a jet engine or rocket, and is then exploded after impact on the target.

The ignition current is supplied to the igniter through the cable, and current flows to each igniter, igniting the igniter, igniting the ignition agent, and initiating the combustion of the propellant. In order to exploit the missile, it is necessary to verify the actual operating cable.

This is because the constant voltage or current is flowed to the igniter in order to explode, and there are variables that can not be ignited depending on the type and condition of the cable.

The main variables are as follows. (1) the allowable current varies depending on the type of the cable cable (AWG), (2) the cable length is long, the line-to-line resistance may occur and the ignition current may be changed, (3) the cable shielding state, There is a variable that will not be exploited because of. In order to verify these parameters, it is necessary to verify the actual operating cable.

There is a 'malfunction test device and method' of the registered patent publication No. 1392223 as a prior art.

Fig. 1 shows a conventional explosion test apparatus.

However, in the conventional 'explosion test apparatus and method', the cable is located in the same space where the new pipe is exploded, and there is a problem that the actual cable can not be used due to the limit of the damage of the cable due to the explosion of the new pipe during the test.

More specifically, in the conventional detonation experiment apparatus shown in FIG. 1, a hole 111 is arranged so that a cable connecting the explosion pipe and the new pipe can pass. However, the cable and the fuse may be located in the same space of the same security mechanism 112, resulting in damage to the detonating cable. Therefore, cables and connectors that are usually fabricated using actual in-flight cables are fabricated and connected, but production costs are incurred and it is not possible to verify the actual missile cables.

1, reference numerals 100 and 101 denote a mounting mechanism, 110 a safety mechanism, 210 a power supply device, and 220 a GUI providing device. The detailed configuration of FIG. 1 can be found in Patent Registration No. 1392223.

Another prior art is the 'Guidance Vehicle Ignition Device and Guided Fire Launching System' of Patent Registration No. 0972122.

FIG. 2 is a view for explaining a process in which the launch device ignites the ignition gun ignition device according to another prior art.

The other prior art shown in FIG. 2 has a limitation in that it does not actually connect the guided car cable but carries out verification of the guided car firing system that applies the detonation signal, and there is a hassle to connect each terminal.

More specifically, FIG. 2 illustrates the squib terminal SQB and the squib return terminal SQB_RTN of the launch device 40 to the terminal 33 of the ignition car igniter 30 to ignite the car charger igniter 30, And connects the squib ready terminal SQB_RDY and the squib ready return terminal SQB_RDY_RTN of the launch device 40 to the terminal 32 of the ignition car igniter 30.

The relay contact connection of the coil relay 31 is switched from CN (dotted line) to CO (solid line) by applying a drive signal for magnetizing the coil of the coil relay 31 through the squib ready terminal SQB_RDY, Both ends of the resistor (RSQB) are opened. Then, a certain amount of current is supplied to the squib resistance RSQB through the squib terminal SQB to ignite the squib resistance RSQB. This connection process is complex and can lead to incorrect connections.

Thus, the conventional technique has a drawback in that it can not be verified with respect to the operating cable.

That is, the conventional technique has a problem that it is not possible to verify the actual operating cable for the ignition (ignition, ignition) or squib test by connecting the mounted joyful carbon cable, and thus it is not possible to secure the ignition in actual operation.

Since it does not use a cable that actually operates, it has a limitation of verification of a device that simply applies an alarm signal.

For example, in the 'Explosion Experimental Apparatus and Method' of the registered patent publication No. 1392223, the cable is located in the same space where the new pipe explodes, so that the new pipe may be detonated during the test and the debris may damage the cable. can not do it.

The method disclosed in Patent Publication No. 0972122, titled 'Guided Carbon Ignition Device and Guided Carbon Launching System', has a limitation to perform only verification of the guided car launching system that applies the squib signal without actually connecting the guided car cable.

Verification of actual operating cables is essential.

Patent Document 1: Japanese Patent Registration No. 1392223 (Registered on Apr. 29, 2014) Patent Document 2: Registration No. 0972122 (Registered on Jul. 19, 2010)

SUMMARY OF THE INVENTION It is an object of the present invention to provide an aeronautical test apparatus and method for verifying a missile caravan cable which can verify a cable disposed in a real missile without the hassle of connecting or removing a connector and a line, and can reliably verify a missile cable.

According to an aspect of the present invention for achieving the above object, the present invention provides an ignition system for an internal combustion engine, And a ignition box that is adapted to prevent cables and detonating fragments of the detonator from splashing out.

The ignition box includes a connector for connecting the guide car cable and the igniter, a connector fixing fixture at one end in the longitudinal direction of the ignition box and fixing the connector, and a shape for covering the entire connector, And a debris blocking member for preventing the debris from splashing out.

The connector fixture may be a pair of rubber fixtures which are fixedly attached to both sides of the connector.

The connector fixing jig may be movable in a direction perpendicular to the longitudinal direction of the ignition box by the moving means at one longitudinal end portion of the ignition box.

Wherein the moving means includes a rail portion provided at one longitudinal end portion of the ignition box in a direction perpendicular to the longitudinal direction and a pair of movable rods which are movable on the rail portion and on which the connector fixing fixture is fixed, And a fixing unit for fixing a state in which the rod moves the rail portion.

Wherein the rail portion is a rail having a moving hole through which the moving rod is movable and the fixing portion is a fixing nut fastened to the moving rod, the moving rod being disposed and moved through the moving hole, the connector fixing fixture being fixed at one end, And the fixing nut is fastened to the other end of the through-hole so that the rail portion can be fixed.

The rail portion may be made of stainless steel.

The debris blocking member may have a frusto-conical shape that wraps around the tip of the connector and has a larger diameter in the direction of the protector from the tip of the connector, and may be made of a metal material.

Both ends of the debris blocking member may be fixed to the blocking member fixing jig provided in the ignition box via an elastic body.

A protective cover may be disposed at a portion of the guide tube cable that is connected to the connector so as to surround the guide tube cable.

The protective cover may be disposed at the same position as the connector fixed to the connector fixture by being fixed to the fixing portion.

The protective cover may be a mesh-type cylindrical tube.

The protective cover may be made of stainless steel.

The igniter has an igniter that receives an electrical signal from one side and ignites the explosive to cause an explosion.

When the ignition signal is applied in the missile launch system, it is an explosion test method for verifying the missile test cable that is applied to the explosive device through the in-flight wiring of the missile, and connecting the connector connected to the missile cable to the explosive device And fixing the connector.

The step of securing the connector includes moving the movable rod along the rail portion provided in the ignition box to cover the entire connector with the fragment blocking member provided in the ignition box, And fixing the connector fixing fixture fixing the connector and the debris blocking member surrounding the connector to each other.

Connecting a protective cover of a cylindrical shape through which the joyful carbon cable passes to a moving rod fastened with the fixing nut to protect the joyful carbon cable after the fixing of the connector, And a step of applying an aerial signal in the guided vehicle launching system.

The present invention is characterized in that after an explosive device is disposed in the ignition box and a connector of the missile cable is connected to the explosive device, a debris blocking structure such as a debris blocking member or a protective cover is applied to prevent the explosive fragments of the explosive device from splashing out It is possible to prevent the damage of the guide car cable caused by the small debris.

In particular, the present invention protects the entire guided car cable by flexibly fixing the guided car cave so that the detonated pieces do not jump out of the ignition box.

Therefore, according to the present invention, it is possible to carry out the explosion test by putting the actual guided car cable into the ignition box without any additional connection, and it is possible to verify the reliability without damaging the guided car cable which is the in-car wiring.

1 is a conceptual view showing an external device (a) connected to an experimental apparatus of a conventional fuse and a safety mechanism (b) for accommodating the fuse.
BACKGROUND OF THE INVENTION 1. Field of the Invention [0001] The present invention relates to an ignition device,
Fig. 3 is a schematic view showing an apparatus for testing a missile in accordance with the present invention.
FIG. 4 is a schematic view showing a fragmentation ignition ignition box for an aeronautical test device for verifying a guided car cable according to the present invention. FIG.
5 is a view for explaining a detonation test apparatus for verifying a guided car cable according to the present invention, showing a configuration for securing a connector.
FIG. 6 is a view showing a detonation test apparatus for verifying a guided car cable according to the present invention, in which a protective cover is connected to a fixing part. FIG.

Hereinafter, embodiments of the present invention will be described in detail with reference to the accompanying drawings.

The aeronautical test apparatus for verifying a missile caravan cable of the present invention is an aeronautical test apparatus for verifying a missile caravan cable which is subjected to an aerial explosion test when a signal is applied to an aerial device through an in-car wiring of a guided car when an aerial signal is applied thereto.

FIG. 3 is a block diagram showing an apparatus for testing a missile caravan cable according to the present invention, and FIG. 4 is a configuration diagram showing a scratch-shielding ignition box for a test apparatus for verifying a missile caravan cable according to the present invention have.

3, the apparatus for testing a missile caravan cable according to the present invention includes a missile launch system 10, a missile charger cable 40 and an ignition box 50.

The missile launch system 10 generates an electromagnetic pulse from a radar at a certain distance and applies an aerial signal to the missile 20. The missile launch system 10 may be a multi-function radar.

When an ignition signal is applied to the guide gun 20, a constant voltage or current is applied to the igniter 30 through the in-tile wiring, so that the detonator 30 is ignited. The missile 20 may receive an aerial signal through the internal antenna. The guided missile 20 may be guided at the component stage.

The igniter (30) is coupled to a igniter that receives an ignition signal at one side and ignites a gunpowder to cause an explosion. The igniter 30 is ignited by an igniter that receives an electrical ignition signal, and the propellant is burnt and explosive pressure is generated.

The missile cable 40 is an in-tank wiring of the missile 20 and transmits a signal applied from the missile launch system 10 to the exploder 30. Precisely, the missile cable 40 transmits the signal applied from the missile launch system 10 to the igniter coupled to the igniter 30, and the igniter 30 is ignited by ignition of the igniter.

The ignition box 50 serves to prevent splattering of the igniter 30 from splashing out and to protect the entire guide cylinder cable 40. The ignition box 50 may have a cylindrical shape or a rectangular shape with an internal space and may be made of a metal material. For example, the ignition box can be made of steel or stainless steel to withstand high temperatures and high pressures.

The ignition box 50 is configured to protect the connector fixing fixture 70 that fixes the connector 60 in cooperation with the debris blocking member 90 to be described later.

So that the igniter 30 is disposed in the internal space of the ignition box 50.

The ignition box 50 is provided with a connector 60 for positioning the igniter 30 in the internal space and connecting the igniter 30 to the guide cylinder cable 40, a connector fixing fixture 70, a debris blocking member 90, .

The connector 60 connects the jumper cable 40 to the igniter 30 and the connector fixing fixture 70 fixes the connector 60 connected to the igniter 30. The connector 60 connects the connector, which is actually connected to the jumper cable 40, to the igniter 30.

The connector fixing fixture 70 is disposed at one end in the longitudinal direction of the ignition box 50. The connector fixing fixture 70 is a pair of rubber fixtures which come in close contact with both sides of the connector 60 to fix the connector 60. [ The connector fixing fixture 70 employs a rubber material to prevent the gap between the connector 60 and the debris blocking member 90 from being generated.

The prevention of the occurrence of the gap between the connector 60 and the debris blocking member 90 is intended to protect the guided car cable 40 from the small fragments.

The pair of connector fixture 70 is movable in the direction perpendicular to the longitudinal direction of the ignition box 50 by the moving means 80 at one longitudinal end portion of the ignition box 50, .

The moving means 80 enables the connector fixing fixture 70 to move in the form of a rail in a floating manner so that the connector 60 can be fixed.

The connectors 60 are different in size and different in size according to the type of the guide cam cable 40. Therefore, the connector fixing fixture 70 is moved and fixed by moving it so as to prevent the fragments in the ignition box 50 from escaping to the outside of the ignition box 50. This is to protect the entire missile cable 40.

Fig. 5 is a view showing a configuration for fixing a connector in the aeronautical test device for verifying a missile caravan cable according to the present invention.

5, the moving means 80 includes a rail portion 81, a moving rod 83, and a fixing portion 85. As shown in Fig.

The rail portion 81 is installed at one longitudinal end portion of the ignition box 50 in a direction perpendicular to the longitudinal direction of the ignition box 50. The moving rods 83 are paired to be movable in the rail 81, and the connector fixing fixture 70 is fixed to each end. The fixing portion 85 fixes the state in which the moving rod 83 has moved from the rail 81.

The fixed part 85 is a fixed nut 85 which is coupled to the moving rod 83. The fixed part 85 is a part of the movable part 83, The movable rod 83 can be a cylindrical rod, and a connector fixing fixture 70 is fixed to one end of the cylindrical rod, and a screw thread is formed at the opposite end thereof, so that the fixing nut 85 can be fastened.

The connector fixing fixture 70 can be integrally fixed in such a manner that it is fitted to one end of the moving rod 83 and attached thereto.

The moving rod 83 is moved to the moving hole 82 of the rail 81 and the connector fixing fixture 70 is integrally fixed to one end and the fixing nut 85 is fastened to the other end thread, The moved state can be fixed.

The moving rod 83 is provided with a latching portion 86 which is hooked on the rail 81 at one side of the outer circumferential surface and the state in which the latching portion 86 and the fixing nut 85 interact with each other to move the rail 81, . For example, the moving rod 83 is restricted by the engaging portion 86 when the other end of the moving rod 83 is exposed through the moving hole 82 to the lower portion of the rail 81, 85 can be fixed by moving the rail portion.

The engaging portion 86 may be a supporting nut coupled to the outer circumferential surface of the moving rod 83. For example, the latching portion 86 may be a support nut coupled to the outer circumferential surface of the moving rod 83 that does not pass through the moving hole 82 of the rail portion 81. In this case, the support nut and the fixing nut may interact with each other to fix the moving rod 83 to the rail 81.

The rail portion 81 is made of a stainless steel material capable of withstanding high temperature and high pressure.

The debris blocking member 90 has a shape that wraps around the entirety of the connector 60 and functions to prevent splashing of the detonator 30 from splashing out.

The debris shielding member 90 is formed in a frusto-conical shape that wraps around the tip of the connector 60 to be engaged with the detonator 30 and widens in the direction of the detonator 30 from the tip of the connector 60, and is made of a metal material.

The debris blocking member 90 is fixed to the blocking member fixing jig 91 provided on the ignition box 50 via the elastic member 93 on both sides of the outer surface. The elastic body 93 may be a coil spring having a high density. The elastic body 93 applies an elastic force to the debris shielding member 90.

The blocking member fixing fixture 91 is a fixture for fixing the fragment blocking member 90 and the fragment blocking member 90 is fixed to the blocking member fixing fixture 91 through the coil spring 93 having a high density.

The debris shielding member 90 is fixed to both sides of the connector 60 by fixing the nut 85 to the moving rod 83. When the connector fixing fixture 70 is fixed to both sides of the connector 60, Can be moved.

At this time, the rubber jig 70 serves to remove the gap between the connector 60 and the debris blocking member 90. The blocking member fixing jig 91 is made of a steel material so as to withstand the heat and pressure during the explosion.

When the connector 60 of the in-car guided missile cable 40 is connected to the thruster 30, there is no process of connecting the test cable manufactured separately, so that the convenience of installation is increased and the human operator Reduces the possibility of error and improves the reliability of the explosion test to verify missile cables.

In addition, there is an advantage of cost reduction since it is not necessary to separately manufacture a test cable or a connector.

And a protective cover 95 for protecting the explosion-proof guided-gas cable 40 is further provided.

FIG. 6 is a view showing a state where the protective cover is connected to the fixing part in the apparatus for testing a missile caravan cable according to the present invention.

6, the protective cover 95 is disposed at a portion where the guide car cable 40 is connected to the connector 60 so as to cover and protect the guide car cable 40 in a spaced-apart manner. The protective cover 95 is for protecting the guided-fiber cable 40 in the event that a small debris is splashed. The protective cover 95 is capable of accommodating a plurality of guided carbon cables 40 due to its shape.

The protective cover 95 may be disposed at the same position as the connector 60 fixed to the fixing portion 85 and fixed to the connector fixing fixture 70. When the protective cover 95 is disposed at the same position (on the same line) as the connector 60, it is possible to protect the guide car cable 40 more efficiently.

The protective cover 95 is a cylindrical tube of mesh type and made of a stainless steel material resistant to high temperature and high pressure.

The safety of the explosion test is improved by safely accommodating a plurality of in-flight guidance cable 40 with the protective cover 95.

On the other hand, when the ignition signal is applied by the ignition car firing system 10, the ignition test method for verifying the guided car cable using the ignition test device for verifying the guided car cable described above is applied to the igniter 30 via the in- The method of the present invention includes the steps of connecting a connector 60 connected to a joyful carbon cable 40 to an explosive device 30 disposed in a ignition box 50, To the ignition box (50).

The step of fixing the connector 60 to the ignition box moves the moving rod 83 along the rail 81 provided on the ignition box 50 so that the connector fixing fixture 70 at one end of the moving rod 83 is moved to the connector 60 So that the debris blocking member 90 provided in the ignition box 50 surrounds the entirety of the connector 60. In this case,

The step of fixing the connector 60 to the ignition box may be performed by fixing the state in which the movable rod 83 moves the rail portion 81 by fastening the fixing nut 85 to fix the connector 60 70 and the debris blocking member 90 surrounding the connector 60 are fixed.

For example, after the movable rod 83 is moved in the rail portion 81 so that the debris blocking member 90 covers the entirety of the connector 60, the movable member 83 is moved downward through the movable hole 82 of the rail portion 81 The fixing nut 85 is fastened to the exposed moving rod 83 so that the connector fixing fixture 70 surrounding the connector 60 and the debris blocking member 90 are prevented from moving.

At this time, since the connector fixing fixture 70 closely fixes both sides of the connector 60 while supporting the state in which the debris shielding member 90 surrounds the connector 60, the gap between the connector 60 and the debris shielding member 90 Thereby preventing occurrence.

6, after the step of securing the connector 60, a cylindrical protective cover 95 through which the guide cylinder cable 40 passes is inserted into the fixing nut 85 to protect the guide cylinder cable 40 To the moving rod 83 which is fastened.

Next, a step of applying the detonating signal in the ignition car firing system 10 is performed so that the detonator 30 disposed in the ignition box 50 is detonated.

If the exploding operation is smoothly performed by the above step, the reliability of the joyful carbon cable is verified.

With the above-described configuration, it is possible to carry out the explosion test by putting the actual touring car cable into the ignition box as it is without further connection, thereby verifying the reliability of the touring car cable which is the in-car wiring.

The operation of the present invention will be described below.

In the operation of the present invention, the exploratory test process for verifying a missile caravan cable will be described.

In order to carry out the explosion test for the verification of the missile cable, first the detonator 30 is disposed in the ignition box 50 and the connector is connected to the detonator 30. The connector 60 is fixed by the connector fixing fixture 70.

The connector fixing fixture 70 is in close contact with both sides of the connector 60 and is moved by the movement of the moving rod 83 to determine the position of the connector 60, (30).

The moving rod 83 is moved along the rail 81 provided on the ignition box 50 and is fixed by a fixing nut 85 which is fastened to the outer circumferential surface. The spacing is adjusted corresponding to the size of the connector 60.

The fragmental blocking member 90 surrounding the connector 60 is provided in the ignition box 50. The fragmental blocking member 90 is fixed to the blocking member fixing fixture 91 through a coil spring having a high density, 60 in the direction of the arrow.

When the connector fixing fixture 70 fixes the connector 60, the debris blocking member 90 cooperates with the ignition box 50 to protect the connector fixing fixture 70.

When the connector fixing fixture 70 fixes the connector 60, the connector fixing fixture 70 serves to remove the gap between the connector 60 and the fragment blocking member 90, 40).

A protective cover 95 for protecting the missile cable 40 is connected to the ignition box 50. The protective cover 95 is connected to the ignition box 50 in such a manner that the inner surface of the protective cover 95 is hooked on the fixing nut 85 so that the joyful carbon cable 40 passes through the protective cover 95, 60, respectively.

That is, when the protective cover 95 is connected to the portion fastened with the fixing nut 85, the test preparation is completed.

When the test preparation of the aerial test device for guided car cable inspection is completed by the above-described procedure, the configuration shown in Fig. 3 is obtained.

When an ignition signal is applied in the guidance car firing system 10, a signal is applied to the igniter through the actual in-flight wiring. That is, the ignition signal applied from the ignition car emission system 10 is received by the antenna of the guided car 20 and transmitted to the igniter 30 through the guided car cable 40, which is an in-car wiring.

The detonating signal is received at an igniter coupled integrally to the detonator 30 and ignites the detonator 30 by burning the propellant while igniting the igniter.

Explosion of the explosion device 30 causes explosion of large and small pieces of debris, which are prevented by the ignition box 50 and the debris blocking member 90 from splashing out, .

In addition, since the protective cover 95 protects the guide car cable 40 from small pieces, damage to the guide car cable 40 can be prevented.

When the ignition is smoothly progressed in the above-described ignition test process, the reliability of the guided-carburetor cable 40 is verified.

The present invention described above is a system in which a signal is applied to an explosion device 30 through an actual in-floor wiring when an ignition and ignition signal is applied in the stimulus carbon emission system 10, 50) and tested.

In addition, since the types of cable connector types are various, it is possible to fix the connector 60 by moving the connector fixing fixture 70 fluidly.

The connector fixing fixture 70 can protect the entire guide cylinder cable 40 by flexibly fixing the connector 60 so that fragments can not escape out of the ignition box 50 during the explosion.

The debris blocking member 90 can secure the connector 60 and protect the connector fixing fixture 70 from debris.

The protective cover 95 is a safety device for preventing the debris from splashing out of the ignition box 50, and a plurality of guided carbon cables 40 are accommodated. Even if small fragments are splashed during the detonation, the guide car cable 40 can be protected through the protective cover 95.

The connector fixing fixture 70 can be moved by the moving means 80 in a fluid manner to fix the connector 60 and fix the debris blocking member 90.

The debris shielding member 90 can be moved to the size of the connector 60 in a fluid manner when the connector fixing fixture 70 fixes the connector 60 through the coil spring having a high density.

Further, the connector fixing fixture 70 is in the form of a rubber to remove a gap between the connector 60 and the debris blocking member 90.

The above-described configuration protects the explosion-proof guided-gas cable 40 from debris to prevent damage.

As described above, according to the present invention, it is possible to carry out the actual explosion test by inserting the actual missile car cable into the ignition box 50 without further connection, thereby verifying the reliability without damaging the missile car cable 40, which is the in-car wiring.

In other words, it is possible to verify the guide cylinder cable 40 disposed in the actual guidance cam 20 without the hassle of connecting or removing the connector 60 and the guide cam cable 40.

The method is simple and cost effective and can perform real missile cable verification that has not been attempted in the prior art.

Best Mode for Carrying Out the Invention The present invention has been described with reference to the drawings and the specification. Although specific terms are used herein, they are used for the purpose of describing the present invention only and are not used to limit the scope of the present invention described in the meaning of the claims or the claims. Therefore, it is to be understood that the present invention may be embodied in many other specific forms without departing from the spirit or essential characteristics thereof. Accordingly, the true scope of the present invention should be determined by the technical idea of the appended claims.

10: Guided-fire launch system 20: Guided-fire
30: Explosive device 40: Guidance cable
50: ignition box 60: connector
70: Connector fixture (rubber fixture)
80: moving means 81:
82: moving ball 83: moving rod
85: fixing part (fixing nut) 86: engaging part (supporting nut)
90: Debris blocking member 91: Blocking member fixing jig
93: elastic body (coil spring) 95: protective cover

Claims (17)

delete A missile launch system that applies an aerial signal to a missile;
A joyful carbon cable which is an in-tank wiring of the guided car and transmits a signal applied from the guided car firing system to an igniter; And
A ignition box to prevent the explosive debris of the igniter from splashing out;
/ RTI >
The ignition box
A connector for connecting the guide car cable and the detonator;
A connector fixing fixture provided at one end in the longitudinal direction of the ignition box and fixing the connector; And
A debris blocking member which has a shape that wraps around the entire connector and prevents splashed pieces of the detonator from splashing out;
And a test apparatus for verifying the test jig cable. The method of claim 2,
Wherein the connector fixture is a pair of rubber fixtures which are fixedly attached to both sides of the connector. The method of claim 3,
The connector fixture
Is movable in a direction perpendicular to a longitudinal direction of the ignition box by a moving means at one longitudinal end portion of the ignition box. The method of claim 4,
The moving means
A rail portion provided at one longitudinal end portion of the ignition box in a direction perpendicular to the longitudinal direction;
A pair of movable rods that are movable on the rails and to which the connector fixing fixture is fixed at respective ends; And
A fixing part fixing the moving rod in a state of moving the rail part;
And a test apparatus for verifying the test jig cable. The method of claim 5,
Wherein the rail portion is a rail having a moving hole capable of moving the moving rod, and the fixing portion is a fixing nut fastened to the moving rod,
Wherein the moving rod is moved through the moving hole and is fixed, the connector fixing fixture is fixed at one end and the fixing nut is fastened to the other end penetrating the moving hole to fix the moving state of the rail portion. Vibration test equipment for verification. The method of claim 5,
Wherein the rail portion is made of a stainless steel material. The method of claim 2,
The debris blocking member
Wherein the connector has a truncated cone shape that wraps around the tip of the connector and has a diameter widened from the tip of the connector toward the protector, and is made of a metal material. The method of claim 8,
The debris blocking member
And both ends thereof are fixed to a blocking member fixing jig provided on the ignition box via an elastic body. The method of claim 5,
And a protective cover is disposed on a portion of the guide tube cable that is connected to the connector so as to surround the guide tube cable in a spaced manner. The method of claim 10,
Wherein the protective cover is fixed to the fixing portion and is disposed at the same position as the connector fixed to the connector fixing fixture. The method of claim 10,
Wherein the protective cover is a mesh-type cylindrical tube. The method of claim 12,
Wherein the protective cover is made of a stainless steel material. A missile launch system that applies an aerial signal to a missile;
A joyful carbon cable which is an in-tank wiring of the guided car and transmits a signal applied from the guided car firing system to an igniter; And
A ignition box to prevent the explosive debris of the igniter from splashing out;
/ RTI >
Wherein the igniter has an igniter for igniting a gunpowder and generating an explosion by receiving an electrical signal at one side thereof. delete This is an explosion test method for the verification of the missile car cable that the signal is applied to the detonator through the in-car wiring of the missile when the detonation signal is applied in the missile launch system,
Connecting the connector connected to the missile cable to the detonator arranged in the ignition box; And
Securing the connector;
/ RTI >
The step of securing the connector
Moving the moving rod along a rail portion provided in the ignition box to enclose the whole of the connector in a fragile blocking member provided in the ignition box;
Fixing the moving rod in a state of being fixed by a fixing nut to fix the connector fixing fixture for fixing the connector and the debris blocking member surrounding the connector;
And a second step of performing an aerial test for verifying the guided car cable. 18. The method of claim 16,
After securing the connector,
Connecting a protective cover of a cylindrical shape through which the guide car cable passes to a moving rod having the fixing nut fastened to protect the guide car cable; And
Applying an ignition signal in the ignition char combustion system such that the detonator disposed in the ignition box is ignited;
Wherein said step of performing the aerial test comprises the steps of:

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