Separation device of ejector motor for portable missile

摘要

Disclosed is a separation device (100) of an ejector motor (130) for a portable missile (1), capable of being separated from a missile (1) without any additional separation devices after ejecting the missile (1). An ejection rocket motor (130) and a separation device are integrally formed. Ejection is performed by a thrust generated while the ejection rocket motor (130) is combusted, and separation is performed by cutting off shearing bolts (113) with using a force generated from a separation cylinder (141) when the combustion of the ejection rocket motor (130) has been completed. This operation and configuration may minimize a weight and a space occupied by a general ejection and separation device (100) in a missile system.