Vehicle having a ceramic radome affixed thereto by a compliant m

Aeronautics and astronautics – Aircraft structure – Fuselage and body construction

Patent

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Details

244131, 438606, 75134N, 2281245, B64C 114

Patent

active

058848649

ABSTRACT:
A missile has a body with a substantially circular nose opening therein, and a ceramic radome sized to cover the nose opening. A compliant metallic circular transition element is disposed structurally between the radome and the body. The transition element includes an elongated compliant arm region and a crossbar region positioned adjacent to the radome such that a lower margin surface of the radome rests against an upper side of the crossbar region. A brazed butt joint is formed between the lower margin surface of the radome and the upper side of the crossbar region of the transition element. A second brazed lap joint is formed between the vehicle body and the elongated compliant arm of the transition element.

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patent: 5691736 (1997-11-01), Hunn et al.

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