A rocket includes a front warhead, a rear propellant actuator, and a propulsion enhancement arrangement which comprises at least two propulsion impulse generators longitudinally cascadedly mounted between the warhead and the rear propellant actuator, wherein each propulsion impulse generator compris
A rocket includes a front warhead, a rear propellant actuator, and a propulsion enhancement arrangement which comprises at least two propulsion impulse generators longitudinally cascadedly mounted between the warhead and the rear propellant actuator, wherein each propulsion impulse generator comprises a storage barrel for storing a predetermined amount of explosive materials to provide propelling impulse upon controlled explosion thereof, and a time-internal control arrangement comprising a time-interval control device mounted on a bottom of the front warhead, a time-interval trigger wire operatively connected with the time-interval control device, and at least two time-interval triggers mounted along the time-interval trigger wire and inside of each of the storage chambers respectively, wherein the time-interval triggers trigger the explosion of the explosive material stored in the storage chamber from the bottom propelling impulse generator to the top propelling impulse generator one by one at a predetermined time intervals, so as to further propels the front warhead to the predetermined position at a predetermined velocity and after each explosion.
대표청구항▼
What is claimed is: 1. A rocket, comprising: a front warhead; a rear propellant actuator for generating propelling force to propel said front warhead in a predetermined orientation and at a predetermined speed; and a propulsion enhancement arrangement which comprises: at least two propulsion impuls
What is claimed is: 1. A rocket, comprising: a front warhead; a rear propellant actuator for generating propelling force to propel said front warhead in a predetermined orientation and at a predetermined speed; and a propulsion enhancement arrangement which comprises: at least two propulsion impulse generators longitudinally cascadedly mounted between said front warhead and said rear propellant actuator, wherein each propulsion impulse generator comprises: a storage barrel having a periphery side wall, a bottom wall, and a top ceiling forming a storage chamber therein, wherein one propulsion impulse generator is adapted to be mounted on another propulsion impulse generator, so that all propulsion impulse generators are connected together to be mounted between said front warhead and said rear propellant actuator; a predetermined amount of explosive material selected from a group consisting of trinitrotoluene which is stored in said storage chamber and enclosed by a foam material to retain a spherical shape in said storage chamber to provide propelling impulse upon controlled explosion thereof, wherein said predetermined amount of explosive material is arranged for propelling said front warhead to a predetermined position; and a time-interval control arrangement comprising a time-interval control device mounted on a bottom of said front warhead, a time-interval trigger wire operatively connected with said time-interval control device, and at least two time-interval triggers mounted along said time-interval trigger wire and inside of each of said storage chambers respectively, wherein a predetermined set of parameters is put into said time-interval control device to control a time interval of a first explosion and following explosions, wherein said time interval generates a propelling impulse, wherein said time-interval triggers trigger an explosion of said explosive material stored in said storage chamber from said propelling impulse generator in bottom to said propelling impulse generator in top one by one at a predetermined time interval, so as to further propel said front warhead to a predetermined position at a predetermined velocity after each explosion, wherein said periphery side wall extends upwardly forming a tubular valley above said top ceiling, said tubular valley above said top ceiling has an inner threaded wall at an inner side of said periphery side wall, and said bottom wall extends downwardly to protrude beyond a bottom end of said periphery side wall, said protruding part of said bottom wall has an outer thread wall, which is adapted for matching said inner threaded wall at said inner side of said periphery side wall, so that one propulsion impulse generator is capable of mounting on another propulsion impulse generator by threaded connection, wherein said explosion detaches said threaded connection between said bottom wall of said propulsion impulse generator which is exploding and said periphery side wall, and then generates said propelling impulse which further propels said rocket, wherein said propelling impulse is further strengthened by said peripheral side wall of said propulsion impulse generator which is exploding, wherein said peripheral side wall is tubular shaped to guide bursted gas. 2. The rocket, as recited in claim 1, wherein said time interval is 0.1-1 s. 3. The rocket, as recited in claim 2, said bottom wall of said storage barrel is thicker in centre comparing to a thickness of said bottom wall at edge, in such a manner that said bottom wall avoids being destroyed but is detached from said threaded connection by said explosion, so as to strengthen said propelling impulse by said peripheral side wall which is tubular shaped. 4. The rocket, as recited in claim 1, said bottom wall of said storage barrel is thicker in centre comparing to a thickness of said bottom wall at edge, in such a manner that said bottom wall avoids being destroyed but is detached from said threaded connection by said explosion, so as to strengthen said propelling impulse by said peripheral side wall which is tubular shaped. 5. A propulsion enhancement system for a rocket comprising a front warhead and a propellant actuator adapted for propelling said warhead, wherein said propulsion enhancement system comprises: at least two propulsion impulse generators longitudinally cascadedly mounted between said front warhead and said rear propellant actuator, wherein each propulsion impulse generator comprises: a storage barrel having a periphery side wall, a bottom wall, and a top ceiling forming a storage chamber therein, wherein one propulsion impulse generator is adapted to be mounted on another propulsion impulse generator, so that all propulsion impulse generators are connected together to be mounted between said front warhead and said rear propellant actuator; a predetermined amount of explosive material selected from a group consisting of trinitrotoluene which is stored in said storage chamber and enclosed by a foam material to retain a spherical shape in said storage chamber to provide propelling impulse upon controlled explosion thereof, wherein said predetermined amount of explosive material is arranged for propelling said front warhead to a predetermined position; and a time-interval control arrangement comprising a time-interval control device mounted on a bottom of said front warhead, a time-interval trigger wire operatively connected with said time-interval control device, and at least two time-interval triggers mounted along said time-interval trigger wire and inside of each of said storage chambers respectively, wherein a predetermined set of parameters is put into said time-interval control device to control a time interval of a first explosion and following explosions, wherein said time interval generates a propelling impulse, wherein said time-interval triggers trigger an explosion of said explosive material stored in said storage chamber from said propelling impulse generator in bottom to said propelling impulse generator in top one by one at a predetermined time interval, so as to further propel said front warhead to a predetermined position at a predetermined velocity after each explosion, wherein said periphery side wall extends upwardly forming a tubular valley above said top ceiling, said tubular valley above said top ceiling has an inner threaded wall at an inner side of said periphery side wall, and said bottom wall extends downwardly to protrude beyond a bottom end of said periphery side wall, said protruding part of said bottom wall has an outer thread wall, which is adapted for matching said inner threaded wall at said inner side of said periphery side wall, so that one propulsion impulse generator is capable of mounting on another propulsion impulse generator by threaded connection, wherein said explosion detaches said threaded connection between said bottom wall of said propulsion impulse generator which is exploding and said periphery side wall, and then generates said propelling impulse which further propels said rocket, wherein said propelling impulse is further strengthened by said peripheral side wall of said propulsion impulse generator which is exploding, wherein said peripheral side wall is tubular shaped to guide bursted gas. 6. The rocket, as recited in claim 5, wherein said time interval is 0.1-1 s. 7. The rocket, as recited in claim 6, said bottom wall of said storage barrel is thicker in centre comparing to a thickness of said bottom wall at edge, in such a manner that said bottom wall avoids being destroyed but is detached from said threaded connection by said explosion, so as to strengthen said propelling impulse by said peripheral side wall which is tubular shaped. 8. The rocket, as recited in claim 5, said bottom wall of said storage barrel is thicker in centre comparing to a thickness of said bottom wall at edge, in such a manner that said bottom wall avoids being destroyed but is detached from said threaded connection by said explosion, so as to strengthen said propelling impulse by said peripheral side wall which is tubular shaped. 9. A rocket, comprising: a front warhead; a rear propellant actuator for generating propelling force to propel said front warhead in a predetermined orientation and at a predetermined speed; and a propulsion enhancement arrangement which comprises: at least two propulsion impulse generators longitudinally cascadedly mounted between said front warhead and said rear propellant actuator, wherein one propulsion impulse generator is adapted to be mounted on another propulsion impulse generator, so that all propulsion impulse generators are connected together to be mounted between said front warhead and said rear propellant actuator, wherein a predetermined set of parameters is put into each of said propulsion impulse generator to control a timing and an elevation in air of an explosion that generates a propelling impulse, wherein each propulsion impulse generator comprises: a storage barrel having a periphery side wall, a bottom wall, and a top ceiling forming a storage chamber therein; and a predetermined amount of explosive material selected from a group consisting of trinitrotoluene which is stored in said storage chamber and enclosed by a foam material to retain a spherical shape in said storage chamber to provide propelling impulse upon controlled explosion thereof, wherein said predetermined amount of explosive material is arranged for propelling said front warhead to a predetermined position; and a time-sensitive trigger device operatively communicated with said storage chamber, wherein said time sensitive trigger device comprises a timing device and an ignition trigger operatively communicated with each other in order to ignite said explosive material stored in said storage chamber at a predetermined time pre-set to said timing device, wherein said predetermined time pre-set to said timing device of said propulsion impulse generator lower is shorter than said predetermined time pre-set to said timing device of said propulsion impulse generator above, so that when said rocket reaches a timing and elevation in air according to said predetermined set of parameters inputted, said time-sensitive trigger of said propulsion impulse generator on a bottom triggers said explosion of said explosive material stored in said storage chamber, said rear propellant actuator and said propelling impulse generator are separated from said above propelling impulse generator, and one and another, until all said propulsion impulse generator explode, a last propulsion impulse generator are separated from said front warhead, wherein each explosion generates said propelling impulse which further propels said front warhead to said predetermined position at a predetermined velocity after said explosion, wherein said periphery side wall extends upwardly forming a tubular valley above said top ceiling, said tubular valley above said top ceiling has an inner threaded wall at an inner side of said periphery side wall, and said bottom wall extends downwardly to protrude beyond a bottom end of said periphery side wall, said protruding part of said bottom wall has an outer thread wall, which is adapted for matching said inner threaded wall at said inner side of said periphery side wall, so that one propulsion impulse generator is capable of mounting on another propulsion impulse generator by threaded connection, wherein said explosion detaches said threaded connection between said bottom wall of said propulsion impulse generator which is exploding and said periphery side wall, and then generates said propelling impulse which further propels said rocket, wherein said propelling impulse is further strengthened by said peripheral side wall of said propulsion impulse generator which is exploding, wherein said peripheral side wall is tubular shaped to guide bursted gas. 10. The rocket, as recited in claim 9, wherein said time-interval trigger is mounted inside said storage chamber within said explosive material. 11. The rocket, as recited in claim 10, wherein said time interval is 0.1-1 s. 12. The rocket, as recited in claim 11, said bottom wall of said storage barrel is thicker in centre comparing to a thickness of said bottom wall at edge, in such a manner that said bottom wall avoids being destroyed but is detached from said threaded connection by said explosion, so as to strengthen said propelling impulse by said peripheral side wall which is tubular shaped. 13. The rocket, as recited in claim 10, said bottom wall of said storage barrel is thicker in centre comparing to a thickness of said bottom wall at edge, in such a manner that said bottom wall avoids being destroyed but is detached from said threaded connection by said explosion, so as to strengthen said propelling impulse by said peripheral side wall which is tubular shaped. 14. The rocket, as recited in claim 9, wherein said time interval is 0.1-1 s. 15. The rocket, as recited in claim 14, said bottom wall of said storage barrel is thicker in centre comparing to a thickness of said bottom wall at edge, in such a manner that said bottom wall avoids being destroyed but is detached from said threaded connection by said explosion, so as to strengthen said propelling impulse by said peripheral side wall which is tubular shaped. 16. The rocket, as recited in claim 9, said bottom wall of said storage barrel is thicker in centre comparing to a thickness of said bottom wall at edge, in such a manner that said bottom wall avoids being destroyed but is detached from said threaded connection by said explosion, so as to strengthen said propelling impulse by said peripheral side wall which is tubular shaped.
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이 특허에 인용된 특허 (10)
Humphrey,John Morgan, Ballistic target defense system and methods.
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