Propulsion Enhancement Arrangement for Rocket

A propulsion enhancement system for a rocket comprising a 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 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 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-internal 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 time-interval control device to control a time interval of an first explosion and said following explosions that generates a propelling impulse, wherein said time-interval triggers trigger said explosion of said explosive material stored in said storage chamber from said bottom propelling impulse generator to said top propelling impulse generator one by one at a predetermined time intervals, so as to further propels said front warhead to said predetermined position at a predetermined velocity and after each explosion.

A rocket, comprising:

• a front warhead;
• a rear propellant actuator for generating propelling force to propel said 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 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 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 subjacent propulsion impulse generator is shorter than said predetermined time pre-set to said timing device of said above propulsion impulse generator, 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 and after said explosion.