Abstract:
An invention in which a projectile device is deployed from a compressed air firing system that, upon impact of the projectile device into a target, the projectile device embeds itself in the intended target&#39;s outer surface or material. In one application, a GPS receiver and transmitter provided within the projectile device relays position data to a receiving apparatus that is monitored by a stationary or mobile conveyance. In another application, the projectile device, may include remotely operable explosives which are preferably triggered once the target is an area where the explosives can be detonated with minimal collateral damage.

Description:
This Application relates to Provisional Application 61/152,479 Filed 13 Feb. 2009 
    
    
     FIELD OF INVENTION 
     The present invention relates to projectile device for deploying and impaling into a target. 
     BACKGROUND OF INVENTION 
     There is a world wide upsurge in episodes of criminal activity regarding the operation of motorized vehicles, and or mobile mechanical conveyances. Citizens placed in a position of confrontation or under rule of authority for insignificant and/or malicious infractions or crimes deviate from authorized direction by such authorities to cease operation of said conveyances. When they fail to stop, the level of violation and resistance committed is significantly raised. 
     Under a civilian crisis, as in a traffic stop where the violator refuses to cease operation of a vehicle and continues on a course simply away from the pursuing agent of authority, the propensity for intense biological stress upon the operators has been shown to limit logical decision making ability, therefore decreasing concern for self and others. The operator fleeing from authority may take drastic risks to escape detainment, sometimes causing minor to extravagant property destruction, as well as minor to serious injuries, or often taking of a human life. The media and news institutions, as well as federal, state, and local law enforcement agencies have termed these as police chases, or high-speed pursuits. 
     There is a paradigm shift in the law enforcement industry leading toward progressive policy changes in the reduction of the types of crimes committed that permit officers, deputies, troopers, or agents to pursue the suspect in flight. This paradigm shift is a result of the growing public and courtroom disdain of pursuits that kill or maim innocent people. As a direct result of years of policy modifications by departments and agencies all over the world, the general knowledge of such change has spread, and the dilemma of whether to chase or not is debated. 
     There are many devices that attempt to help law enforcement agencies avoid, prevent, and end vehicle pursuits. One of the very first such devices is what are called stop sticks. Stop sticks are a tire deflation device (TDD) that can be deployed several different ways. One way is to have a person near the roadway in front of the vehicle being pursued, and as the vehicle approaches, the person throws the TDD into the roadway directly in the vehicle&#39;s path in hope that the tires run over the deflation spikes. The obvious challenges with this is getting a person positioned ahead of the pursued vehicle, having the person throw the device in the roadway (which the vehicle can steer around it), retrieving the device from the roadway so that other non intended vehicles don&#39;t run over it, the danger of the person deploying the device being struck by the pursued or chase vehicle(s), and the possibility of the chase vehicle after having one or more of its tires deflated losing control and causing a crash. 
     Another way as described in U.S. Pat. No. 6,758,628 by Curry, Jr. is to have the stop sticks mechanically deployed by another pursuit vehicle, so as to avoid a person having to manually deploy the tire deflation device from the side of the road, exposing themselves to danger. However, this still does not solve the challenge of stopping the pursuit as the suspect vehicle can continue on its course of action, now possibly more uncontrollable than before. In addition, technological advances in tire manufacturing have made “run-flat-type” tires available for most vehicles, leaving a tire deflation device unpractical in some circumstances. 
     Another device designed to help eliminate vehicle pursuits is that of an electronic component fired to the suspect vehicle, with the intention of getting it to stick. A gun-type device is placed on the front of a law enforcement vehicle loaded with a device that is fired and designed to apply itself to the vehicle and track its location using GPS sensors from within, and transmitting such data to a receiving party. This technology aides law enforcement in the dilemma of whether or not to pursue, as they may fire the projectile, turn the police vehicle around, and let the suspect vehicle go. The suspect within the pursued vehicle will assume it has avoided capture from law enforcement authorities and presumably will resume normal motor vehicle operation that is less likely to cause a crash. The law enforcement agency tracks the suspect vehicle through use of the devices GPS transmitter located on the back of the vehicle, and plans where, when, and how the law enforcement agency will seize the vehicle in a safe place and take custody of the occupant(s). One such invention is U.S. Pat. No. 7,207,274 by Plew et al. that provides a method and system of firing a projectile comprised of a sticky medium containing a sensor within. They describe that a two-part dielectric gel polymer encased in the tip of the projectile will stick to a target when fired from a weapon, and subsequently transmit many different possibilities of data, depending on its mission and predetermined encased sensor, one being GPS, to a remote receiving apparatus. One of the pitfalls with a sticky substance used at a contact point is that it may not adhere to the targets surface when fired at a high velocity from a vehicle traveling at a very high rate of speed, and that the device houses a heavy payload of electronic equipment making adhesion even more difficult. 
     SUMMARY AND OBJECTS OF THE INVENTION 
     The projectile device is generally a pointed, barbed, cylindrical-shaped steel and aluminum projectile device housing a GPS receiving sensor, a cellular transmission device, and other support electronic devices used to track a vehicle or other conveyance. The data transmitted by the projectile device is relayed to a tracking agency allowing for a planned, and safer tactical capture strategy. Additionally, if munitions or disruptive technology (such as electromagnetic pulse equipment) are carried by the projectile device, armed services and security personnel can use the projectile device to remotely eliminate a target that has been identified within a heavily populated area by tracking the target and waiting until the target is in a location where it is safe to remotely trigger the munitions or other disruptive technology. 
     The present embodiment is of a method and system, for deploying a projectile housing GPS and other related electronic support sensors, from a compressed air system, either mounted from an aimable cannon on a vehicle or from a handheld weapon like device, and impaling the intended targets surface with the retention cross of the fired projectile, and tracking its location with supporting electronic apparatuses. The tip of this projectile has a retention cross that, while impacting the target, decelerates the penetration shaft containing a blank charge, while the outer housing containing a firing pin continues forward, impacting and thus firing the charge, explosively forcing the penetration shaft forward towards the impact point on the targets surface, where the pointed tip penetrates the surface, makes a hole and the barbs of the retention cross catch the lip of the now serrated material around the diameter of the hole, and locks it into place, making removal extremely difficult. 
     In a version designed for GPS tracking and threat elimination, the GPS and other related electronic support sensors and equipment would be complimented with remote activated explosives. Both mediums are intended to track using GPS apparatuses, one for use in law enforcement during high speed pursuits or for intelligence collection, the other with explosives for use with the armed services as a threat elimination device in an area deemed undesirable for the use of explosives, and must wait for the explosives to be detonated. 
     It is an object of this embodiment of the invention to provide a method for attaching a projectile fired from a high powered compressed air cannon at a suspect vehicle, and attaching it with the idea that removal of such projectile is not easy. It is an object of this embodiment to be able to be used during a high speed police chase, with no reasonable limitation of measured speed on a legal roadway. It is an object of this embodiment to eliminate high speed police chases using said embodiment and included GPS tracking systems, and statistically eliminate the chance of causing a crash resulting in property damage, injury, and or death. It is an object of this embodiment, when projectile is loaded with said GPS tracking equipment, and remote activated explosives, to be utilized in an armed forces scenario, specifically in a densely populated area, where a target has been acquired, and the need for the threat to be eliminated, the projectile can be fired by desired cannon to the threat, and subsequently tracked as the vehicle or conveyance retreats away from such a populated area where detonation is less likely to cause collateral damage. It is an object of this embodiment for the invention to cause damage to the target being fired at, allowing for the unique non obvious method of attachment to work. 
    
    
     
       BRIEF DESCRIPTION OF THE DRAWINGS 
         FIG. 1  presents an assembled projectile device with safety pin. 
         FIG. 2  presents a cut away view of the projectile device. 
         FIG. 3  presents an exploded view of the projectile device. 
         FIG. 4  presents a see thru view of the projectile device. 
         FIG. 5  presents the retention cross in a pre-deployment state. 
         FIG. 6  presents the front of the projectile device in a post-deployment state. 
         FIG. 7  presents the vehicle mounted launch system. 
         FIG. 8  presents the handheld launch system. 
         FIG. 9  presents a motor vehicle deploying a projectile device to a target. 
         FIG. 10  presents the front of the projectile device making initial contact with the outer surface of a target. 
         FIG. 11  presents the front of projectile device after penetration of into the target. 
         FIG. 12  presents the projectile device and components of payload bay. 
         FIG. 13  presents the wired electronic medium 
     
    
    
     DRAWING REFERENCE NUMBERS 
       100  Projectile 
       102  Projectile Cut-Away view 
       104  Outer Housing 
       104 A Pay load bay 
       104 B Firing Pin Mounting Hole 
       104 C Safety Hole 
       104 D Interior of the Outer Housing 
       105  Safety Pin 
       108  Cap 
       108 A Cap Threads 
       112  Penetration Shaft 
       112 A Top of Penetration Shaft 
       112 B Upper mid section of Penetration Shaft 
       112 C Lower mid section of Penetration Shaft 
       112 D O-ring Milled Groove 
       112 E Lower section of Penetration Shaft 
       112 F Charge Seat 
       112 G Penetration Shafts&#39; threaded bored tip hole 
       116  Firing Pin 
       118  O-ring, Large 
       119  O-ring, Small 
       120  Blank Cartridge 
       122  Retention Cross 
       124  Pointed Impact Tip 
       124 A Pointed Impact Tip, Threaded Base 
       126  Target Surface Material 
       200  Vehicle Mounted Launch System 
       200 A Laser Targeting Acquisition System 
       200 B Vertical Aiming Apparatus System 
       300  Hand Held Launch System 
       400  Vehicle, Launch/Delivery 
       402  Vehicle, Target 
       500  Wired Electronic Medium Apparatus 
       500 A Switch; Safety Covered, Device Power/Laser Targeting Acquisition 
       500 B Switch; Spring, Controls Vertical Aiming Apparatus System 
       500 C Switch; Firing Actuator 
       600  Blasting Cap and Primary Charge Apparatus 
       602  GPS Receiver/Cellular Transmission Device/Data Retrieval Antennae 
       604  RF Transponder/Remote Sensor/Data Transmitting and Receiving Device 
       606  Power Source (Battery) 
       608  Force Recognition Sensor 
       610  Payload Bay Door 
     DETAILED DESCRIPTION OF THE INVENTION 
     The present invention, as presented in  FIGS. 1-12 , is a projectile device generally comprising an outer containment housing, a penetration shaft extending from the outer containment housing, a tip attached to an end of the penetration shaft, a retention cross attached to the tip, within the outer containment housing is provided a charged round, a firing mechanism having a firing pin, a force recognition sensor, a power source, a data transmission and receiving device, a sensor recognition device and a data retrieval antennae and wherein the projectile device is formed as an aerodynamic cylindrical unit. 
     The projectile device  100  includes a pointed impact tip  124 , a retention cross  122 , a cap  108 , a large O-ring  118 , a small O-ring  119 , a penetration shaft  112 , a blank charge  120 , a firing mechanism including a firing pin  116 , and an outer housing  104 . The safety pin  105  is of a cylindrical shape and size that will fit into the safety pin holes  104 -C to block the firing pin from contacting the blank charge. 
     Some of the individual parts have areas on them that help further define its shape, or purpose, and are described as follows: pointed impact tip threaded base  124 -A, cap threads  108 -A, penetration shaft&#39;s threaded bored tip hole  112 -G, top of the penetration shaft  112 -A, upper mid section of the penetration shaft  112 -B, lower mid section of the penetration shaft  112 -C, milled groove  112 -D, lower section of the penetration shaft  112 -E, charge seat  112 -F, interior of outer housing  104 -D, safety pin holes  104 -C, firing pin mounting hole  104 -B, and payload bay  104 -A. 
     As shown in  FIG. 5 , the retention cross  122  includes, but is not limited to a 4 bladed cross. There are several engineered forms, angles, thicknesses, shapes, lengths, or other undescribed variations or modifications to the retention cross  122 , that will obviously mimic the method of this embodiment, and those skilled in the art will recognize that, and in the spirit of the invention the aforementioned claims relate to the scope and method of the functionality of the embodiment of the retention cross  122 . The purpose of the retention cross  122 , is to provide a method of embodiment to a target where removal of the projectile  100  from said target, is difficult. 
     As shown in  FIG. 12 , the payload bay  104 -A contains a combined unit with a GPS receiver, Cellular Transmission Device/Data Retrieval Antennae  602 , a combined unit with a RF Transponder/Remote Sensor/Data Transmitting and Receiving Device  604 , a power source (battery)  606 , a force recognition sensor  608 , and covered by a payload bay door  610 . The payload bay  104 -A, in another application, contains a blasting cap with primary charge  600 . 
     As shown in  FIG. 7 , is the vehicle mounted launch system  200 , affixed laser targeting acquisition system  200 -A, the Vertical Aiming Apparatus System  200 B. 
     As shown in  FIG. 8  is the Handheld Launch System  300 . 
     As shown in  FIG. 9 , the vehicle  400  that is launching or delivering the projectile device  100 , is shown behind the target vehicle  402 . 
     As shown in  FIG. 10  and  FIG. 11 , the Targets Surface Material, is shown in a before and after image of the projectiles  100  impact. 
     As shown in  FIG. 13 , the Wired Electronic Medium  500  controls the firing of the projectile  100  from the vehicle mounted launching system  200 . The Wired Electronic Medium has a power switch  500 -A, which is a safety covered switch that turns the power on to the projectile  100 , the Vertical Aiming Apparatus  200 -B, and the Laser Targeting Acquisition System  200 -A. There is a Spring Switch  500 -B, that controls the vertical movement of the vehicle mounted launching system  200  through the vertical aiming apparatus  200 -B. There is a Firing Actuator Switch  500 -C, that controls when the projectile  100  is fired from the vehicle mounted launching system  200 . 
     General Assembly Process 
     As shown in  FIG. 1 , the projectile  100  is of a cylindrical shape. As shown in  FIG. 2 , the projectile  100  is shown with the base of the outer housing  104 , wider than the base of the penetration shaft  112 . At the top of the penetration shaft  112 , a retention cross  122 , is secured to the penetration shaft  112 , with the pointed impact tip  124 . The diameter of the base of the penetration shaft  112  is wider than diameter of the upper portion of the penetration shaft  112  (to which the retention cross  122 , and the pointed impact tips&#39; base  124 -A are attached), and is milled to slide down into the interior of the outer housing  104 -D. In the mid section  112 -C of the penetration shaft  112 , there is a milled groove  112 -D for placement of an O-ring  118 , which assists in a snug fit into the outer housing  104 , and the expansion of gases during the blank charge  120  firing process. 
     In the bottom of the outer housing  104 , there is a firing pin  116 , which is secured by means of adhesive bonding to the firing pin mounting hole  104 -B. 
     The bottom of the penetration shaft  112 , has a hole milled in the center called a charge seat  112 -F, wherein, a blank charge  120  is placed, with the rim of the blank charge  120  wider than the diameter of the charge seat  112 -F, so as not to let the rim of the blank charge  120  insert completely into the charge seat  112 -F, thus leaving the rim of the blank charge  120 , exposed, and nearly flush with the bottom of the penetration shaft  112 . This design will allow for proper firing of the blank charge  120 , which is a rim firing .25 caliber blank cartridge. In this described embodiment projectile  100 , a rim fire cartridge is utilized to drive the penetration shaft  112  forward. Other embodiments may utilize a center fire cartridge, and may not be limited to any particular cartridge type or caliber. Different embodiments require different performance characteristics inherent to different cartridge types and sizes. 
     The penetration shaft  112 , along with blank charge  120 , O-ring  118 , retention cross  122 , and the pointed impact tip  124 , are placed into the outer housing  104 , with a small distance left between the firing pin  116 , and the bottom of the blank charge  120 . A small series of safety pin holes  104 -C are bored into the mid section of the outer housing  104 , and allow for a safety pin  105  to be inserted for safe handling of loaded projectile  100 . The safety pin  105  is primarily used during maintenance, loading, unloading, training, or other unforeseeable operational manipulation while removed from the vehicle projectile launch system  200  (See  FIG. 7 ), or a handheld projectile launch system  300  (See  FIG. 8 ). The safety pin  105  may be provided in different shapes and configurations such as a bolt or other rigid member. The bored safety pin holes  104 -C are also used for the escape of explosive gas and pressure when the penetration shaft  112  moves forward. 
       FIG. 4  shows the outer housing  104 , the cap  108 , and the penetration shaft  112 , as the main body components of the projectile  100 . When the penetration shaft  112 , is inserted into the outer housing  104  with a blank charge  120 , the fit is snug, and with the O-Ring  118  in place in the milled groove  122 -D allows for a gas tight seal between the parts, which prevents gas leakage after firing of the blank charge  120 . If the distance between the walls of the penetration shaft  112 , and the walls of the outer housing  104  is too large, then during firing of the blank charge  120 , the gases that are created would pass through the gap between said walls instead of forcing the penetration shaft  112  forward and into the target vehicle  402 . 
     The cap  108 , screws down onto the outer housing  104 , after the penetration shaft  112  is placed into the outer housing  104 . The penetration shaft  112 , has a smaller diameter near the front  112 -A, a larger diameter just behind it  112 -B, an even larger diameter towards the mid and rear sections  112 -C, and  112 -E, and a groove  112 -D separating sections  112 -C, and  112 -E. The groove  112 -D is where the O-ring  118  is inserted to ensure a proper seal. The interior diameter of the hole at the top of the cap  108 , has a slightly larger diameter than the penetration shafts&#39;  112  section  112 -B. Since the diameter of the penetration shafts  112  section  112 -C, and section  112 -E, is larger than the hole at the top of the cap  108 , the penetration shaft  112  will not pass completely through the hole in the cap  108 . The smaller diameter of the penetration shafts  112  section  112 -A, allows for the retention cross  122 , under stress of penetration to a targets outer material, to bend backwards towards the penetration shaft  112  section  112 -A. 
     Referring to  FIG. 4 , the assembly process of the embodiment projectile  100  is done in the following order: firing pin  116  is attached to the firing pin mounting hole  104 -B at the center of the base inside of the outer housing  104 ; a blank charge  120  is placed into the bored hole called the charge seat  112 -F at the center of the bottom of the penetration shaft  112 ; an O-ring  118  is placed into the groove section  112 -D of the penetration shaft  112 ; the penetration shaft  112  is then placed into the outer housing  104 ; another O-ring  119  is placed around the base of the penetration shaft  112  section  112 -B; the cap  108  is then placed onto the threads of the outer housing  104 , and the cap threads  108 -A are tightened down; the retention cross  122  is then placed on top of the penetration shaft  112  section  112 -A; the hole in the center of the retention cross  122 , and the hole in the center of the penetration shafts  112  section  112 -A, are of the same diameter, and are lined up. In the tip of the penetration shaft  112  section  112 -A, there is a threaded bored tip hole  112 -G. The threaded tip base  124 -A of the pointed impact tip  124 , then slides down into the matched up holes of the center of the retention cross  122 , and the tip of the penetration shafts  112  section  112 -A, and screws in to the tip hole  112 -G. The means of attachment of the pointed impact tip  124 , and tip base  124 -A to the penetration shaft  112 , can be done in a multitude of ways including, but not limited to: gluing, chemical weld, mechanical pinning, or threading. As shown in  FIG. 4 , the attachment of the pointed impact tip  124 , and the tip base  124 -A, is secured to the penetration shaft  112  section  112 -A, by way of threading into the threaded tip hole  112 -G. In another means of attachment of the pointed impact tip  124  as described above, the penetration shafts  112  section  112 -A may not have a threaded tip hole  112 -G, but a smooth tip hole  112 -G. 
     Referring to  FIG. 4 , the outer housing  104  has an area behind the location where the firing pin mounting hole  104 -B is located. Access to this area will be made through a door on the outer housing  104  to be designed specifically based on the exact measurements of the electronic equipment, and will change during further development and production, and such access door is not a claim being made on this embodiment. This area is referred to as the payload bay  104 -A. In the payload bay  104 -A, numerous types of electronic sensing and electronic support devises can be placed, including, but not limited to, radio frequency (RF) equipment, a force recognition sensor, power source, data transmission and GPS receiving devices, other sensor recognition devices, data retrieval antennae, and explosive munitions. The payload bay  104 -A may utilize a small layer of force reduction type material just behind the firing pin mounting hole  104 -B to help reduce the amount of G-force the payload experiences during deceleration. In the said projectile  100 , the electronic devices loaded into the payload bay  104 -A may be of many different types, models, and modified for particular missions. Such electronic devices must withstand high G-forces as equations for survivability are paramount in the success of the projectile  100  attaching to its&#39; intended target, and delivering expected data, to the remote or stationary monitoring apparatus(s). The payload of choice is able to be loaded, unloaded, serviced, or repaired through the access door which is to be added during production. The projectile  100  will experience severe G-forces when it is fired from either a compressed air, or round fired system, and said projectile  100  impacts its intended target. 
     For illustrative purposes only, describing the operation, the target in the detailed description, and shown in  FIG. 9 , is that of a vehicle, however it is not limited to such conveyance, as the projectile  100  may be utilized on numerous other unstated targets. 
     Referring to  FIG. 7 , once the projectile  100  has been assembled, it is placed into the barrel of the vehicle mounted launch system  200 . The vehicle mounted launch system  200  is mounted to a pursuit vehicle  400  (See  FIG. 9 ), and is a mechanically aimable device by use of a wired, or wireless remote control from within or outside of pursuit vehicle  400 . 
     Referring to  FIG. 8 , once the projectile  100  has been assembled, it is placed into the barrel of the handheld launch system  300 . The handheld launch system  300  is carried by a person, and can be shoulder or hip fired, aimed by the operator themselves, and fired using a triggering mechanism controlled by a biomechanical digit. 
     The most appropriate launch system, either vehicle mounted launch system  200 , or the handheld launch system  300 , is selected by the operator as it relates to the mission at hand. 
     Use and Operation 
     Referring to  FIG. 9 , an example of a projectile  100  is fired from a pursuit vehicle  400 , utilizing a vehicle projectile launch system  200 , and impacting the target vehicle  402 . In this illustration, the projectile  100  impales the rear of the target vehicle  402 , and the penetration shaft  112 , pointed impact tip  124 , and retention cross  122 , enter the outer layer of the target vehicle  402 . The illustration demonstrates one example, but not limited to, the surface area of the target which the said projectile  100  can be fired at, the type of pursuit vehicle  400  the projectile can be fired from, and the location of the vehicle projectile launching system  200 . 
     Referring to  FIG. 6 , the depicted drawing is that of the front of the projectile  100 , the pointed impact tip  124 , the front of the penetration shaft  112  section  112 -A, and partially  112 -B, and the retention cross  122 . The image is referred to as the front of the projectile with the retention cross in retaining form  128 . The recessed diameter of the penetration shafts  112  section  112 -A is visible, as it will allow for the retention cross  122 , while penetrating the surface of the target, to fold rearward similar as depicted in the drawing, to aide in the reduction of overall diameter of the projectiles  100  diameter at the point of impact, thus allowing for penetration of thick surfaces of a target feasible. 
     Referring to  FIG. 10 , the depicted drawing is that of a perspective view of the front of the projectile  100  in flight, at the point where impact to the targets outer surface  126  is occurring. The retention cross  122  is still in its un-deployed state. 
     Immediately after the projectile  100  makes contact with its&#39; intended target, the penetration shaft  112  is depressed slightly into the outer, housing  104 . This depression causes the blank charge  120 , that is seated into the charge seat  112 -F, to forcefully make contact with the firing pin  116 . Upon contact, the blank charge  120  will fire. The explosive gasses created by the firing of the blank charge  120 , force the penetration shaft  112  forward, towards the target. This explosive force helps to drive the pointed impact tip  124 , and retention cross  122 , deeper into the surface of the target. The penetration shaft  112  stops its forward movement when the lower mid section  112 -C makes contact with the cap  108 . 
     The intention for the use of the blank charge  120  to create a large penetration force, is to ultimately reduce the speed at which the projectile  100  has to be fired from its launch system. Thus allowing for deployment of the projectile  100  to be done so with greater ease than with the use of gun power type firing systems such as grenade launchers, or shotgun shells. 
     Referring to  FIG. 11 , the depicted drawing is that of a perspective view of the front of the projectile  100 , after impact and penetration has been made to a targets surface  126 , where the material of the target has been broken and forced inward by the pointed impact tip, serrating the material around the hole. The retention cross  122 , during penetration, folds rearward, and subsequently after penetration, springs open slightly, catching the serrated material of the hole in the targets surface  126 . After the retention cross  122  catches the material of the target surface  126 , it allows for the back half of the projectile  100 , to remain outside of the target, making optimum use of a clear view of the sky, thus ensuring the GPS, or other receiving and transmitting sensors, have an uninterrupted medium by which to transfer data. 
     The means of deploying the projectile  100  from either the vehicle mounted launch system  200 , or the handheld projectile launch system  300 , includes, but not limited to, utilizing compressed air systems, explosive round fired system, or direct placement system. The detailed descriptions of the types of deployment systems are not included as the principles of the invention relate to its method of application, and tracking system. One type of a compressed air system of deployment utilizes fresh air, a sealed air tank, high pressure air valve, appropriate air fittings, and connects said equipment to a barrel which houses said projectile  100 . A fresh air compressed air system can be filled and refilled easily by the operator from a type of portable or permanent air compressor, using fresh air, without regulation on how many times it can be refilled. Utilization of a pressure relief valve in the compressed air system ensures that over pressurization of the sealed air tank is unlikely, thus reducing the danger of an air tank eruption. Another type of compressed air system of deployment utilizes a sealed and pre manufactured compressed carbon dioxide (CO2) canister, canister puncture system, appropriate air fittings, and connects said equipment to a barrel which houses said projectile  100 . A pre manufactured compressed CO2 canister is small, inexpensive, easily replaced after it is discharged, and will not leak air from its fittings connecting it to the other equipment. The CO2 canister can be pre manufactured to a certain pounds per square inch (PSI), therefore eliminating the need for a pressure relief valve. 
     An explosive round fired system utilizes an explosive burst from a blank cartridge charge placed in a firing sleeve, wherein; the base of the outer housing  104  fits into the sleeve, and the sleeve with the projectile  100  are placed in a barrel, and when detonated by the operator using a remote control apparatus, fires the projectile  100  out of the barrel to its target. There is no detailed description or diagram of this system as it is an example of a type of deployment system that may be utilized. This process is similar to that of a gun, or a gun that fires non lethal projectiles at a target. In this system, there is a barrel, a projectile  100 , a blank charge firing sleeve, a blank charge (similar to illustration of  120 ), and no compressed air systems. The firing sleeve is a sleeve that the projectile  100  fits into, and located at the bottom of such sleeve is a small hole for a blank charge (similar to illustration of  120 ) to be inserted. A raised “floor” in the sleeve allows for the blank round (similar to illustration of  120 ) to sit flush with the bottom of the sleeve, and for the bottom of the embodiment projectile  100  to sit flush with the top of the “floor” near the bottom end of the interior of the sleeve, with the floor being as deep as the blank charge (similar to illustration of  120 ) is tall. Thus when the blank round (similar to illustration of  120 ) is fired in the sleeve by a firing pin device located in the rear of the barrel, the explosion of gases will escape forward into the sleeve forcing the projectile  100  out of the sleeve, out of the barrel, and towards its intended target. 
     In the direct placement system, a moveable mounted arm, extension, or telescoping pole is mounted to the front of a vehicle, and is the delivery system of the projectile  100 . In this direct placement system, the projectile  100  is at the forward most end of the direct placement apparatus, and as the pursuit vehicle  400  closes the gap between it and the target vehicle  402 , the tip of the projectile  100  is exposed from shelter and tapped onto a suitable surface on the target vehicle with an appropriate amount of force to activate the projectiles&#39;  100  blank charge  120  thus activating the said attachment system. In the direct placement system, there is no compressed air system, or blank charge firing system, and the projectile  100  never flies through the air to attach itself to the target vehicle  402  or other undescribed mobile conveyance. 
     The invention presented through drawings, and description, has been done so with particular detail to this embodiment. Variations and modifications of the presented embodiment, that achieve the same results, might be made to those skilled in the art, and it is intended to be covered in the appended claims all such variations and modifications, and that the invention be limited only to the applicable rules of law. All patents cited above are incorporated by reference.