System and method for disabling time critical targets

A system for disabling a time critical target at a site within a geographical area comprising:

• a plurality of ground contacting and spaced apart missile launchers located within or adjacent to the geographical area and disposed in a deployment pattern, each spaced apart mobile missile launcher containing a guided missile and being spaced apart along the ground so that the ground separates adjacent missile launchers, any site within the geographical area being located at a distance from at least one spaced apart missile launcher not more than a maximum distance of travel of a guided missile launched from at least one of the spaced apart missile launchers to the site, the time of travel of a missile from the missile launcher to the site requiring less time than a minimum time available to successfully enable the time critical target at the site;
• wherein the spaced apart missile launchers each comprise a sleeve and a pointed end penetrated into ground at a site, the sleeve at least partially penetrating into the ground and containing the guided missile to be launched from the missile launcher;
• wherein the spaced apart missile launchers each comprise an outer sleeve and an inner sleeve;
• the inner sleeve contains the guided missile and is telescoped relative to the outer sleeve into the ground and contains a battery power unit which maintains the transceiver and the missile in an electrically powered status when embedded in ground;
• the outer sleeve has a fin assembly located proximate to the transceiver;
• and wherein the inner and outer sleeves are guidance paths for launching of the guided missile.

A system for disabling a time critical target at a site within a geographical area comprising:

• a plurality of ground contacting and spaced apart missile launchers located within or adjacent to the geographical area and disposed in a deployment pattern, each spaced apart mobile missile launcher containing a guided missile and being spaced apart along the ground so that the ground separates adjacent missile launchers, any site within the geographical area being located at a distance from at least one spaced apart missile launcher not more than a maximum distance of travel of a guided missile launched from at least one of the spaced apart missile launchers to the site, the time of travel of a missile from the missile launcher to the site requiring less time than a minimum time available to successfully enable the time critical target at the site;
• wherein the spaced apart missile launchers each comprise a sleeve and a pointed end penetrated into ground at a site, the sleeve at least partially penetrating into the ground and containing the guided missile to be launched from the missile launcher;
• at least one sensor, the at least one sensor detecting a time critical target at least one site within the geographical area;
• and
• a command center, linked to the at least one sensor and to the plurality of spaced apart missile launchers, which commands launching of a guided missile from at least one of the spaced apart missile launchers to disable at least one time critical target at least one site detected by the at least one sensor;
• wherein the spaced apart missile launchers each comprise an outer sleeve and an inner sleeve;
• wherein the inner sleeve contains the guided missile and is telescoped relative to the outer sleeve into the ground and contains a battery power unit which maintains the transceiver and the missile in an electrically powered status when embedded in ground;
• wherein the outer sleeve has a fin assembly located proximate to the transceiver;
• and wherein the inner and outer sleeves are guidance paths for launching of the guided missile.

A system for disabling a time critical target at a site within a geographical area comprising:

• a plurality of ground contacting and spaced apart missile launchers located within or adjacent to the geographical area and disposed in a deployment pattern, each spaced apart mobile missile launcher containing a guided missile and being spaced apart along the ground so that the ground separates adjacent missile launchers, any site within the geographical area being located at a distance from at least one spaced apart missile launcher not more than a maximum distance of travel of a guided missile launched from at least one of the spaced apart missile launchers to the site, the time of travel of a missile from the missile launcher to the site requiring less time than a minimum time available to successfully enable the time critical target at the site;
• wherein the spaced apart missile launchers each comprise a sleeve and a pointed end penetrated into ground at a site, the sleeve at least partially penetrating into the ground and containing the guided missile to be launched from the missile launcher;
• wherein the missile launchers located within the geographical area comprise a transceiver with at least an antenna disposed above the ground which transmits a radio signal indicating coordinates thereof within the geographical area and which receives commands for launching the guided missile to disable a time critical target at one site;
• wherein the guided missile contained in the missile launchers contains a guidance system which controls flight of the guided missiles and which is in radio contact with the transceiver or a command center separated from the missile launchers to control flight thereof;
• wherein the spaced apart missile launchers each comprise an outer sleeve and an inner sleeve;
• wherein the inner sleeve contains the guided missile and is telescoped relative to the outer sleeve into the ground and contains a battery power unit which maintains the transceiver and the missile in an electrically powered status when embedded in ground;
• wherein the outer sleeve has a fin assembly located proximate to the transceiver;
• and wherein the inner and outer sleeves are guidance paths for launching of the guided missile.

A system for disabling a time critical target at a site within a geographical area comprising:

• a plurality of ground contacting and spaced apart missile launchers located within or adjacent to the geographical area and disposed in a deployment pattern, each spaced apart mobile missile launcher containing a guided missile and being spaced apart along the ground so that the ground separates adjacent missile launchers, any site within the geographical area being located at a distance from at least one spaced apart missile launcher not more than a maximum distance of travel of a guided missile launched from at least one of the spaced apart missile launchers to the site, the time of travel of a missile from the missile launcher to the site requiring less time than a minimum time available to successfully enable the time critical target at the site;
• wherein the spaced apart missile launchers each comprise a sleeve and a pointed end penetrated into ground at a site, the sleeve at least partially penetrating into the ground and containing the guided missile to be launched from the missile launcher;
• at least one sensor, the at least one sensor detecting a time critical target at least one site within the geographical area;
• and
• a command center, linked to the at least one sensor and to the plurality of spaced apart missile launchers, which commands launching of a guided missile from at least one of the spaced apart missile launchers to disable at least one time critical target at least one site detected by the at least one sensor;
• wherein the missile launchers located within the geographical area comprise a transceiver with at least an antenna disposed above the ground which transmits a radio signal indicating coordinates thereof within the geographical area and which receives commands for launching the guided missile to disable a time critical target at one site;
• wherein the guided missile contained in the missile launchers contains a guidance system which controls flight of the guided missiles and which is in radio contact with the transceiver or a command center separated from the missile launchers to control flight thereof;
• wherein the spaced apart missile launchers each comprise an outer sleeve and an inner sleeve;
• wherein the inner sleeve contains the guided missile and is telescoped relative to the outer sleeve into the ground and contains a battery power unit which maintains the transceiver and the missile in an electrically powered status when embedded in ground;
• wherein the outer sleeve has a fin assembly located proximate to the transceiver;
• and wherein the inner and outer sleeves are guidance paths for launching of the guided missile.

A system for disabling a time critical target at a site within a geographical area comprising:

• a plurality of ground contacting and spaced apart missile launchers located within or adjacent to the geographical area and disposed in a deployment pattern, each spaced apart mobile missile launcher containing a guided missile and being spaced apart along the ground so that the ground separates adjacent missile launchers, any site within the geographical area being located at a distance from at least one spaced apart missile launcher not more than a maximum distance of travel of a guided missile launched from at least one of the spaced apart missile launchers to the site, the time of travel of a missile from the missile launcher to the site requiring less time than a minimum time available to successfully enable the time critical target at the site;
• wherein the spaced apart missile launchers each comprise a sleeve and a pointed end penetrated into ground at a site, the sleeve at least partially penetrating into the ground and containing the guided missile to be launched from the missile launcher;
• wherein the spaced apart missile launchers each comprise an outer sleeve and an inner sleeve;
• wherein the inner sleeve contains the guided missile and is telescoped relative to the outer sleeve into the ground and contains a battery power unit which maintains the transceiver and the missile in an electrically powered status when embedded in ground;
• wherein the outer sleeve has a fin assembly located proximate to the transceiver;
• wherein the inner and outer sleeves are guidance paths for launching of the guided missile;
• and
• the at least one sensor is in the ground within the geographical area.

A system for disabling a time critical target at a site within a geographical area comprising:

• a plurality of ground contacting and spaced apart missile launchers located within or adjacent to the geographical area and disposed in a deployment pattern, each spaced apart mobile missile launcher containing a guided missile and being spaced apart along the ground so that the ground separates adjacent missile launchers, any site within the geographical area being located at a distance from at least one spaced apart missile launcher not more than a maximum distance of travel of a guided missile launched from at least one of the spaced apart missile launchers to the site, the time of travel of a missile from the missile launcher to the site requiring less time than a minimum time available to successfully enable the time critical target at the site;
• wherein the spaced apart missile launchers each comprise a sleeve and a pointed end penetrated into ground at a site, the sleeve at least partially penetrating into the ground and containing the guided missile to be launched from the missile launcher;
• wherein the spaced apart missile launchers each comprise an outer sleeve and an inner sleeve;
• wherein the inner sleeve contains the guided missile and is telescoped relative to the outer sleeve into the ground and contains a battery power unit which maintains the transceiver and the missile in an electrically powered status when embedded in ground;
• wherein the outer sleeve has a fin assembly located proximate to the transceiver;
• wherein the inner and outer sleeves are guidance paths for launching of the guided missile;
• and wherein the at least one sensor is in flight.

An air deployed guided missile assembly comprising:

• a sleeve which is deployed from the air, the sleeve including a pointed end which penetrates the ground upon impact with the ground;
• a guided missile contained within the sleeve with the sleeve guiding the guided missile during launch with the guided missile including a guidance system for guiding flight of the missile in a directed path to a target spaced from a site of the sleeve when penetrated into the ground;
• and
• a transceiver with at least an antenna disposed above the ground after impact which transmits a radio signal indicating coordinates of a location of the guided missile within a geographical area of deployment and which receives commands for launching the guided missile to fly to a site;
• and wherein
• the guided missile has a guidance system which controls flight of the guided missile and which is in radio contact with the transceiver or a command center separated from the deployed missile to control flight thereof.

An air deployed guided missile assembly comprising:

• a sleeve which is deployed from the air, the sleeve including a pointed end which penetrates the ground upon impact with the ground;
• a guided missile contained within the sleeve with the sleeve guiding the guided missile during launch with the guided missile including a guidance system for guiding flight of the missile in a directed path to a target spaced from a site of the sleeve when penetrated into the ground;
• an outer sleeve and an inner sleeve containing the guided missile which is mounted to telescope relative to the outer sleeve and which telescopes upon impact with a ground contact point when deployed from the air;
• and
• a transceiver with at least an antenna disposed above the ground after impact which transmits a radio signal indicating coordinates of a location of the guided missile within the geographical area of deployment and which receives commands for launching the guided missile to fly to a site;
• and wherein
• the guided missile has a guidance system which controls flight of the guided missile and which is in radio contact with the transceiver or a command center separated from the deployed missile to control flight thereof.

An air deployed guided missile assembly comprising:

• a sleeve which is deployed from the air, the sleeve including a pointed end which penetrates the ground upon impact with the ground;
• a guided missile contained within the sleeve with the sleeve guiding the guided missile during launch with the guided missile including a guidance system for guiding flight of the missile in a directed path to a target spaced from a site of the sleeve when penetrated into the ground;
• and
• an outer sleeve and an inner sleeve containing the guided missile which is mounted to telescope relative to the outer sleeve and which telescopes upon impact with a ground contact point when deployed from the air;
• wherein the inner sleeve is telescoped relative to the outer sleeve into the ground and contains a batter power unit which maintains the transceiver and the missile in an electrically powered status when embedded in the ground;
• wherein the outer sleeve has a fin assembly located proximate to the transceiver when the pointed end penetrates into the ground;
• and where the inner and outer sleeves are guidance paths for launching of the guided missile.

An air deployed guided missile assembly comprising:

• a sleeve which is deployed from the air, the sleeve including a pointed end which penetrates the ground upon impact with the ground;
• a guided missile contained within the sleeve with the sleeve guiding the guided missile during launch with the guided missile including a guidance system for guiding flight of the missile in a directed path to a target spaced from a site of the sleeve when penetrated into the ground;
• an outer sleeve and an inner sleeve containing the guided missile which is mounted to telescope relative to the outer sleeve and which telescopes upon impact with a ground contact point when deployed from the air;
• and
• a transceiver with at least an antenna disposed above the ground after impact which transmits a radio signal indicating coordinates of a location of the guided missile within the geographical area of deployment and which receives commands for launching the guided missile to fly to a site;
• wherein the guided missile has a guidance system which controls flight of the guided missile and which is in radio contact with the transceiver or a command center separated from the deployed missile to control flight thereof;
• wherein the inner sleeve is telescoped relative to the outer sleeve into the ground and contains a batter power unit which maintains the transceiver and the missile in a powered status when embedded in the ground;
• wherein the outer sleeve having a fin assembly located proximate to the transceiver when the pointed end penetrates into the ground;
• and wherein the inner and outer sleeves are guidance paths for launching of the guided missile.

A system for disabling a moving target within a geographical area comprising:

• a plurality of ground contacting and spaced apart missile launchers located within or adjacent to the geographical area and disposed in a deployment pattern, each spaced apart mobile missile launcher containing a guided missile and being spaced apart along the ground so that the ground separates adjacent missile launchers, any moving target within the geographical area being located at a distance from at least one spaced apart missile launcher not more than a maximum distance of travel of a guided missile launched from at least one of the spaced apart missile launchers to a calculated position within the geographical area at which at least one guided missile is to fly to disable the moving target;
• at least one sensor, the at least one sensor detecting the moving target within the geographical area;
• at least one processor for calculation of a site to which at least one guided missile is commanded to fly to disable the moving target;
• a command center separated from the missile launchers, linked to the at least one sensor and to the plurality of spaced apart missile launchers, which commands launching of a guided missile from at least one of the spaced apart missile launchers to disable the moving target at site calculated by the at least one processor in response to the detected moving target detected by the at least one sensor;
• and
• an unmanned aircraft which illuminates the time critical target with a beam of light;
• wherein the guided missile includes a sensor which senses reflection of the beam of light from the time critical target and guides, in response to the sensed reflection of the beam of light, the missile during flight to the time critical target.

A system for disabling a moving target within a geographical area comprising:

• a plurality of ground contacting and spaced apart missile launchers located within or adjacent to the geographical area and disposed in a deployment pattern, each spaced apart mobile missile launcher containing a guided missile and being spaced apart along the ground so that the ground separates adjacent missile launchers, any moving target within the geographical area being located at a distance from at least one spaced apart missile launcher not more than a maximum distance of travel of a guided missile launched from at least one of the spaced apart missile launchers to a calculated position within the geographical area at which at least one guided missile is to fly to disable the moving target;
• at least one sensor, the at least one sensor detecting the moving target within the geographical area;
• at least one processor for calculation of a site to which at least one guided missile is commanded to fly to disable the moving target;
• and
• a command center separates from the missile launchers, linked to the at least one sensor and to the plurality of spaced apart missile launchers, which commands launching of a guided missile from at least one of the spaced apart missile launchers to disable the moving target at site calculated by the at least one processor in response to the detected moving target detected by the at least one sensor;
• wherein the spaced apart missile launchers each comprise a sleeve and a pointed end penetrated into ground at a site, the sleeve at least partially penetrating into the ground and containing the guided missile to be launched from the missile launcher;
• wherein the spaced apart missile launchers each comprise an outer sleeve and an inner sleeve;
• wherein the inner sleeve contains the guided missile and is telescoped relative to the outer sleeve into the ground and contains a battery power unit which maintains the transceiver and the missile in an electrically powered status when embedded in ground;
• wherein the outer sleeve has a fin assembly located proximate to the transceiver;
• and wherein the inner and outer sleeves are guidance paths for launching of the guided missile.

A system for disabling a moving target within a geographical area comprising;

• a plurality of ground contacting and spaced apart missile launchers located within or adjacent to the geographical area and disposed in a deployment pattern, each spaced apart mobile missile launcher containing a guided missile and being spaced apart along the ground so that the ground separates adjacent missile launchers, any moving target within the geographical area being located at a distance from at least one spaced apart missile launcher not more than a maximum distance of travel of a guided missile launched from at least one of the spaced apart missile launchers to a calculated position within the geographical area at which at least one guided missile is to fly to disable the moving target;
• at least one sensor, the at least one sensor detecting the moving target within the geographical area;
• at least one processor for calculation of a site to which at least one guided missile is commanded to fly to disable the moving target;
• and
• a command center separated from the missile launchers, linked to the at least one sensor and to the plurality of spaced apart missile launchers, which commands launching of a guided missile from at least one of the spaced apart missile launchers to disable the moving target at site calculated by the at least one processor in response to the detected moving target detected by the at least one sensor;
• wherein the spaced apart missile launchers each comprise a sleeve and a pointed end penetrated into ground at a site, the sleeve at least partially penetrating into the ground and containing the guided missile to be launched from the missile launcher;
• wherein the missile launchers located within the geographical area comprise a transceiver with at least an antenna disposed above the ground which transmits a radio signal indicating coordinates thereof within the geographical area and which receives commands for launching the guided missile to disable the moving target;
• wherein the guided missiles contained in the missile launchers contain a guidance system which controls flight of the guided missiles and which is in radio contact with the transceiver or the command center to control flight thereof;
• wherein the spaced apart missile launchers each comprise an outer sleeve and an inner sleeve;
• wherein the inner sleeve contains the guided missile and is telescoped relative to the outer sleeve into the ground and contains a battery power unit which maintains the transceiver and the missile in an electrically powered status when embedded in ground;
• wherein the outer sleeve has a fin assembly located proximate to the transceiver;
• and wherein the inner and outer sleeves are guidance paths for launching of the guided missile.

A method for disabling a moving target within a geographical area comprising:

• air deploying a plurality of ground contacting and spaced apart missile launchers located within or adjacent to the geographical area and disposed in a deployment pattern, each spaced apart mobile missile launcher containing a guided missile and being spaced apart along the ground so that the ground separates adjacent missile launchers, any moving target within the geographical area being located at a distance from at least one spaced apart missile launcher not more than a maximum distance of travel of a guided missile launched from at least one of the spaced apart missile launchers to a calculated position within the geographical area at which at least one guided missile is to fly to disable the moving target;
• providing at least one sensor to detect the moving target;
• detecting with the at least one sensor the moving target within the geographical area;
• providing a command center, separated from and linked to the at least one sensor and to the plurality of spaced apart missile launchers;
• using at least one processor to calculate a site to which the moving target is calculated to be moving and to which at least one guided missile is commanded to fly to disable the moving target;
• commanding, with the command center, launching of at least one guided missile from at least one of the spaced apart missile launchers which is guided to a site calculated by the at least one processor in response to the detection of the moving target to disable the moving target at the site;
• providing an unmanned aircraft which illuminates the time critical target with a beam of light;
• and
• providing the guided missile with a sensor which senses reflection of the beam of light from the time critical target and guiding, in response to the sensed reflection of the beam of light, the missile during flight to the time critical target.