DETACHABLE HEAD Russian patent published in 2012 - IPC F42B12/58 F42B12/62 

FIELD: rocket technology.

SUBSTANCE: separable rocket head comprises a casing, a frame with a tubular guide, and cylindrical destructive agents with a braking parachute system. The braking parachute systems of each destructive agent are different one from the other with reference to the parachute canopy area and to their structural composition. The extreme destructive agent located at the tubular guide cut to the direction of the departure from the separable head part is equipped with a braking parachute with the maximum canopy area. The braking parachute systems of each following destructive agent are equipped with the same type braking parachutes with least canopy area or with the same canopy area as the preceding agent but they do not comprise a unit for temporary delay in parachute deployment to its opening position. The degree of decrease in the parachute canopy area and in the time of temporary delay in parachute deployment to its opening position are established judging from the obtained destructive agents scattering afield, in the target area. The destructive agents in the tubular guide are mostly orientated towards the departure direction with their point side. The braking parachute systems are located in the rear side of the destructive agents.

EFFECT: enhanced combat effectiveness of the head.

1 dwg, 1 dwg