Fiber optics assembly

In a control system for rolling missiles or the like having a seeker head including an optical system and a heat sensitive detector assembly;

• said optical system including a primary reflecting means, a secondary reflecting means, a reticle/lens assembly, and a fiber optics assembly operatively associated with said reticle/lens assembly, said reticle/lens assembly including a light chopping means, said fiber optics assembly being positioned between said secondary reflecting means and said light chopping means, said fiber optics assembly comprising a disc of optical fibers having an axial cone therein, said cone having an apex which is directed away from said light chopping means.

In a control system for rolling missiles or the like having a seeker head including an optical system and a heat sensitive detector assembly;

• said optical system including a primary reflecting means, a secondary reflecting means, a reticle/lens assembly, and a fiber optics assembly operatively associated with said reticle/lens assembly, said reticle/lens assembly including a pair of light chopping means, said fiber optics assembly being positioned between said pair of light chopping means, said fiber optics assembly comprising a disc of optical fibers, said disc having a central bore therethrough, and a bundle of optical fibers having a tipped cone configuration positioned in said central bore.

In an optical system, a fiber optics assembly comprising a disc of optical fibers having an opaque axial cone therein, said fibers being of substantially the same length and extending in a rearwardly diverging direction, said axial cone having an apex, said apex extending in a direction toward the incidence surface of said disc, said optical fibers having a diameter in the range between 2 and 10 microns.

In an optical system, a fiber optics assembly comprising a disc of optical fibers, said disc having a central bore therethrough, said fibers of said disc being of substantially the same length and positioned substantially parallel with respect to one another, and a bundle of optical fibers having a tipped cone configuration positioned in said central bore, said optical fibers having a diameter in the range between 2 and 10 microns.

In an optical system having a primary reflecting means, a secondary reflecting means, a reticle/lens assembly, and a detector assembly;

• a fiber optics assembly operatively associated with said reticle/lens assembly, said fiber optics assembly including optical fibers having a diameter in the range between 2 and 10 microns, said fiber optics assembly being constructed to translate images appearing near the optical axis to a radially displaced point on said reticle/lens assembly, whereby more efficient chopping of the image by said reticle/lens assembly can occur.

In an optical system having a primary reflecting means, a secondary reflecting means, a reticle/lens assembly, and a detector assembly;

• a fiber optics assembly operatively associated with the reticle/lens assembly, said fiber optics assembly including optical fibers having a diameter in the range between 2 and 10 microns, said optical fibers forming a disc-like member having an opaque axial cone with an apex directed toward the incidence surface of said disc-like member.

In an optical system having a primary reflecting means, a secondary reflecting means, a reticle/lens assembly, and a detector assembly;

• a fiber optics assembly operatively associated with the reticle/lens assembly, said fiber optics assembly including optical fibers having a diameter in the range between 2 and 10 microns, said optical fibers forming a disc-like member having a central bore extending therethrough, and a tipped cone configuration within said central bore of said disc-like member.

In a rolling missile having control means therefor including a heat sensitive seeker head which incorporates an optical system to pass incident energy to a detection assembly which converts the energy into electrical pulses which are utilized to control the missile, the improvement comprising a fiber optics assembly being constructed and operatively associated with the optical system to translate boresight images from said optical system to a radially displaced point on a chopping means of said detection system, whereby control pulses are continuously provided.

In a rolling missile having a control means therefor including a heat sensitive seeker head which incorporates an optical system to pass incident energy to a detection assembly which converts the energy into electrical pulses which are utilized to control the missile, the improvement comprising a fiber optics assembly operatively associated with the optical system to translate boresight images from said optical system to said detection system, said fiber optics assembly including a first bundle of optical fibers forming a disc-like member having a central bore, and a second bundle of optical fibers forming a tipped cone-like member and positioned in said central bore, whereby control pulses are continuously provided.

In a rolling missile having control means therefor including a heat sensitive seeker head which incorporates an optical system to pass incident energy to a detection assembly which converts the energy into electrical pulses which are utilized to control the missile, the improvement comprising a fiber optics assembly operatively associated with the optical system to translate boresight images from said optical system to said detection system, said fiber optics assembly including a bundle of optical fibers forming a disc-like member having an axial cone therein, said cone having an apex directed toward the incidence surface of said disc-like member, whereby control pulses are continuously provided.