Satellite inspection system using hovering-type interceptors

Claim 1

A satellite inspection system for use in hovering-type satellite interceptors comprising: an electro-optical camera in a satellite interceptor having image tube means for receiving the reflected rays of an object in space and for producing electrical outputs representative of the object from the beam scanning readout of the image tube means, said electro-optical camera being a matrix camera having the focal plane thereof divided into quarter sections, each quarter section having an auxiliary lens to focus the image of an object on said camera image tube thereby providing four matrices, each with a resolution equivalent to the resolution of the image tube scanning system; means coupled to said camera for stabilizing same and for receiving guidance signals on an input thereto; a high intensity flash light source coupled to said camera to expose intercepted objects to light for reflection of the object on said camera image tube means; a data transmitter coupled to said electrical outputs of said camera image tube means for transmitting said electrical outputs as electromagnetic signals; a low gain antenna coupled to said transmitter for transmitting said electromagnetic signals groundward; a fuzing proximity switching signal input coupled to said flash light source and to said data transmitter to cause flash light and transmission activity when an object is intercepted at a predetermined range; a ground receiver station remote from said interceptor having a high gain antenna directed to receive the transmission from said satellite interceptor; and an electro-optical receiver in said ground receiver station for transforming said electromagnetic signals into an optical image of said intercepted object whereby rapid televised information of an intercepted object in space is relayed to ground for observation.