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 an upper crossbar region positioned adjacent to the radome such that the lower margin surface of the radome is adjacent to 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 butt joint is formed between the vehicle body and the lower side of a lower crossbar region joined to the arm region. The brazed joints are formed with a single active braze alloy which permits the entire joining operation to be accomplished in a single furnace cycle.