美国空军/波音公司的“ALCM-B”空中发射巡航导弹的尾部在“ALGM-A”结构的基础上进行了重新设计,以便减少阻力、减小雷达横截面积和红外线特性。“A”型有一个缩短的尾部,因为它需要与旋转发射架配合,该发射架是为装美国空军/波音公司的“近程攻击导弹”而设计的。“A”型缩短的尾部使“近程攻击导弹”的旋转发射架的支撑板上有余隙空间。另外,“B”型采用了钝头体头部,这可改善导弹的气动特性,导弹的弹长也增加到6.32米。第一发“B”型飞行试验 The tail of the USAF / Boeing ALCM-B air-launched cruise missiles was redesigned on the ALGM-A structure to reduce drag and reduce radar cross-sectional area and infrared characteristics. The “A” has a shortened tail as it needs to mate with a revolving launcher designed to fit the U.S. Air Force / Boeing “short-range attack missile.” The shortened “A” tail allows for space for clearance on the support plate of the “launcher” revolving launcher. In addition, the “B” type uses a blunt body head, which improves the aerodynamic characteristics of the missile, missile missile length also increased to 6.32 meters. The first “B” type flight test