| 摘要 |
PROBLEM TO BE SOLVED: To provide a payload separation device of a missile that can separate a payload from an aerial propulsion device without using any powder with light and simple structure. SOLUTION: In the payload separation device of a missile, an aerial propulsion device 3 is provided at the rear of a payload 2 such as an underwater cruising body for composing a missile 1, and the payload 2 is separated from the aerial propulsion device 3 when the missile 1 lands on the water. The device is provided with a support band 12 for clamping the payload 2 and the aerial propulsion device 3 by surrounding them from the peripheral direction and a band stopper 21 for fixing the support band 12 while being engaged to it, retaining the connected state between the payload 2 and the aerial propulsion device 3, and at the same time canceling the clamping of the support band 12 while breaking away from the support band 12 due to a fluid pressure being received when the missile 1 lands on the water.
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