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本发明提供了在制动发射条件下消除发射箱中导弹周围的热量的系统和方法。导弹发射箱有一中空的壁，并且在内侧壁上配置了许多分配孔，冷却剂箱经冷却剂输入口与发射箱壁相通，当出现制动发射条件时，导弹底部产生燃气，此时，导弹仍被制动在发射箱内，燃气压力冲击在冷却剂箱挠性面上，使冷却剂箱的容积减小，从而促使冷却剂进入发射壁，并从分配孔喷出。
The present invention provides systems and methods for eliminating heat around a missile in a launch tank under braking launch conditions. The missile launching box has a hollow wall and a plurality of distributing holes are arranged on the inner side wall. The coolant box is communicated with the launching box wall through the coolant inlet, and when the brake launching condition occurs, the bottom of the missile generates gas. At this time, the missile Still being braked in the firing box, the gas pressure impinges on the flexible face of the coolant box, reducing the volume of the coolant box, causing the coolant to enter the firing wall and out of the dispensing hole.