FIELD: spatial apparatus engineering. SUBSTANCE: multi-stage missile has stages and propelling engine connected by coupling modules, head rocket fairing made like cap end closed envelope with transverse uncoupling plane adjacent to final stage of missile and opposite to closed cap end, joining units of head rocket fairing fastening at rocket stage and head rocket fairing disjointing device for missile uncoupling, same time head rocket fairing envelope is made composed by parts with additional uncoupling transverse plane situated at middle site of envelope body. EFFECT: higher operation reliability while head rocket fairing throwing down. 20 cl, 14 dwg
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