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Weapon launching rockets and method to use the same

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专利汇可以提供Weapon launching rockets and method to use the same专利检索,专利查询,专利分析的服务。并且A weapon including in combination, a rocket launcher and a gun attached to said launcher with its axis parallel to that of the launcher to move with said rocket launcher, an artillery tracer projectile for firing from said gun constructed to be crushed upon impact with a target to deposit tracer material thereon which continues to burn, and a rocket provided with guidance means for following said tracer projectile through the entirety of its path to impact the position of said deposited tracer material, wherein said guidance means comprises means rotating the rocket about its axis through its trajectory and at least two guidance devices each including a pair of aerodynamic flaps externally and symmetrically arranged on the rocket about an axial plane and independently movable, a lens positioned on said rocket with its optical axis parallel to the axis of the rocket to receive radiant energy from said tracer material as the rocket is launched to follow the path of said projectile, two radiant energy detector cells each symmetrically placed upon two equal sectors of one circle located in the focal plane of said lens with planes identical to that of the corresponding said aerodynamic flaps, insulating sectors smaller than said detector cells spaced between the cells on said circle, amplifiers coupled to the two cells, and control means responsive to the amplifiers for moving said corresponding flaps proportional to the currents generated in the respective detector cells.,下面是Weapon launching rockets and method to use the same专利的具体信息内容。

1. A weapon including in combination, a rocket launcher and a gun attached to said launcher with its axis parallel to that of the launcher to move with said rocket launcher, an artillery tracer projectile for firing from said gun constructed to be crushed upon impact with a target to deposit tracer material thereon which continues to burn, and a rocket provided with guidance means for following said tracer projectile through the entirety of its path to impact the position of said deposited tracer material, wherein said guidance means comprises means rotating the rocket about its axis through its trajectory and at least two guidance devices each including a pair of aerodynamic flaps externally and symmetrically arranged on the rocket about an axial plane and independently movable, a lens positioned on said rocket with its optical axis parallel to the axis of the rocket to receive radiant energy from said tracer material as the rocket is launched to follow the path of said projectile, two radiant energy detector cells each symmetrically placed upon two equal sectors of one circle located in the focal plane of said lens with planes identical to that of the corresponding said aerodynamic flaps, insulating sectors smaller than said detector cells spaced between the cells on said circle, amplifiers coupled to the two cells, and control means responsive to the amplifiers for moving said corresponding flaps proportional to the currents generated in the respective detector cells.
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