Truss Reinforced Radome Crown Structure Shock Absorbing And Recoiling Sysytem

A truss reinforced radome crown structure shock absorbing and recoiling system for mounting antenna adapter plates or other satellite communication (SAT COM) structures to an aircraft fuselage and allowing for pressurized expansion and contraction of the fuselage, wherein said system is comprised of an actuating recoiling strut including:

• a) a housing comprising a female receiver with a first end having an opening, a second end having an opening with internal threads, an external surface, an internal channel, and a male cap with a first end having an opening to an internal threaded cavity, a second end with an external threaded section and having an opening to an internal channel, and an external surface, wherein the opening on said female receiver is dimensioned to accept the external threaded section on said male cap, wherein said female receiver and said male cap are maintained together by screwing said male cap's external threaded section into the opening with internal threads on said female receiver's second end, and
• b) an actuating rod that is located within said housing and comprises a first end having an opening, and a second end, wherein said actuating rod is slideably situated within said housing's internal channels, and said rod's second end terminates at the end of said male cap's internal channel, wherein a length of said rod extends within said male cap's internal channel, a length of said rod is within and extends through the internal channel on said female receiver, and the first end of said rod outward from the opening on said female receiver's first end, wherein within the opening on said rod is a spherical bearing, and surrounding said rod is a compression spring, wherein said spring facilitates the actuating movement of said rod within and extending from said housing.