Thermal Energy Radiance Expander

Abstract

A specially design missile system use for hindering the centrifugal forces inside vortexes commonly known as tornados. The missile system composed of a typical modified vehicle with a design platform. The platform is design of the insides of a platform that contains liquid and compressed gas. A command and control module and a projectile missile system complement above the platform. When a super cell appears and probable starting of tornado activity commences the Thermal Energy Radiance Expander system is send over to the targeted area. As the initial start of the tornado commences the vehicle and whole system is sent to the target area. The missile is then loaded with the gaseous element turn live and launch on to the target. The missile control through the command module explodes intentionally at the side of the vortex. The aim of the system is to break and hinder further activity of the vortex hence terminating tornado.

1 . Process for delimiting a tornadic event from continuity by means of utilizing high explosives. A method of using a mobile means to confront developing weather patterns that contributes to vortex anomalies. Process uses electronic technology as a means to give user inform decision to confront anomaly. The use of an automated mobile missile system developed for a purpose to attach the vortex anomaly, comprising:
 A mobile system design specifically for the purpose targeting a weather pattern whereby a developing weather pattern develops and the radar-employed system will inform of current abrupt weather anomaly;   Processing electronic system able to capture and analyze a weather anomaly commonly known as thunderstorm within a super cell. The radio detection and ranging is able to inform user. The electronic system is use to target weather anomaly;   An automated missile system use for abruptly delimiting a rising vortex anomaly, the automated missile system is for annihilating a developing vortex; and   Control missiles send to targeted vortex anomaly by remote control to the vortex area. The missile contains a rocket system that is able to accelerate rampantly toward the targeted area. The rocket system is made powerful enough that it is able to accelerate through high volatile winds onto target. The missile contains a specially design fuselage with ample quantities of high explosives. The explosives are integrated onto design in order to explode in a shape manner as to dismantle vortex. The shape explosion is initiated by remote control.   
     
     
         2 . Process for delimiting a tornadic event from continuity according to  claim 1 , wherein said mobile unit provides mobility toward targeted weather anomaly. 
     
     
         3 . Process for delimiting a tornadic event from continuity according to  claim 1 , wherein said mobile system contains electronic technology able to give intelligent decision making by use of RADAR. 
     
     
         4 . Process for delimiting a tornadic event from continuity according to  claim 1 , wherein said mobile unit provides a battery system for rapid deployment in targeted area. 
     
     
         5 . Process for delimiting a tornadic event from continuity by means of utilizing high explosives. A method of using a mobile means to confront developing weather patterns that contributes to vortex anomalies. Process uses electronic technology as a means to give user inform decision to confront anomaly. The use of an automated mobile missile system developed for a purpose to attach the vortex anomaly, comprising:
 A mobile system design specifically for the purpose targeting a weather pattern whereby a developing weather pattern develops and the radar-employed system will inform of current abrupt weather anomaly;   Processing electronic system able to capture and analyze a weather anomaly commonly known as thunderstorm within a super cell. The radio detection and ranging is able to inform user. The electronic system is use to target weather anomaly;   An automated missile system use for abruptly delimiting a rising vortex anomaly, the automated missile system is for annihilating a developing vortex; and   Control missiles send to targeted vortex anomaly by remote control to the vortex area. The missile contains a rocket system that is able to accelerate rampantly toward the targeted area. The rocket system is made powerful enough that it is able to accelerate through high volatile winds onto target. The missile contains a specially design fuselage with ample quantities of high explosives. The explosives are integrated onto design in order to explode in a shape manner as to dismantle vortex. The shape explosion is initiated by remote control.   
     
     
         6 . Process for delimiting a vortex from growth according to  claim 5 , wherein said RADAR system gathers data/information for interpretation for personnel. 
     
     
         7 . Process for delimiting a tornadic event from continuity according to  claim 5 , wherein said information attained by radar is use for analysis. 
     
     
         8 . Process for delimiting a tornadic event from continuity according to  claim 5 , wherein said RADAR works with electronic technology in battery system. 
     
     
         9 . Process for delimiting a tornadic event from continuity by means of utilizing high explosives. A method of using a mobile means to confront developing weather patterns that contributes to vortex anomalies. Process uses electronic technology as a means to give user inform decision to confront anomaly. The use of an automated mobile missile system developed for a purpose to attach the vortex anomaly, comprising:
 A mobile system design specifically for the purpose targeting a weather pattern whereby a developing weather pattern develops and the radar-employed system will inform of current abrupt weather anomaly;   Processing electronic system able to capture and analyze a weather anomaly commonly known as thunderstorm within a super cell. The radio detection and ranging is able to inform user. The electronic system is use to target weather anomaly;   An automated missile system use for abruptly delimiting a rising vortex anomaly, the automated missile system is for annihilating a developing vortex; and   Control missiles send to targeted vortex anomaly by remote control to the vortex area. The missile contains a rocket system that is able to accelerate rampantly toward the targeted area. The rocket system is made powerful enough that it is able to accelerate through high volatile winds onto target. The missile contains a specially design fuselage with ample quantities of high explosives. The explosives are integrated onto design in order to explode in a shape manner as to dismantle vortex. The shape explosion is initiated by remote control.   
     
     
         10 . Process for delimiting a tornadic event from continuity according to  claim 9 , wherein said battery system is set deployment to targeted area. 
     
     
         11 . Process for delimiting a tornadic event from continuity according to  claim 9 , wherein said battery system is set live by personnel. 
     
     
         12 . Process for delimiting a tornadic event from continuity according to  claim 9 , wherein said missile is launch to targeted area. 
     
     
         13 . Process for delimiting a tornadic event from continuity according to  claim 9 , wherein said missile contains a powerful rocket engine. 
     
     
         14 . Process for delimiting a tornadic event from continuity according to  claim 9 , wherein said missile contains a power rocket engine that enable rocket penetrate high winds. 
     
     
         15 . Process for delimiting a tornadic event from continuity according to  claim 9 , wherein said missile is control towards vortex. 
     
     
         16 . Process for delimiting a tornadic event from continuity according to  claim 9 , wherein said rocket explodes by remote control inside vortex. 
     
     
         17 . Process for delimiting a tornadic event from continuity according to  claim 9 , wherein said missile explodes in a shape according to missile. 
     
     
         18 . Process for delimiting a tornadic event from continuity according to  claim 9 , wherein said explosion is of a magnitude that inhibit a tornadic event from continuity.