FIELD: tactical missile and missile-space weapon, as well as commercial missile-space vehicles. SUBSTANCE: the essence of the invention consists in the fact that during the take-off and in the cruise path of the ramjet ejector missile-carrier two ejecting and one ejected flows are produced, the ejected flow and one ejecting flow are oppositely swirled and interact in the reverse flow conditions, which results in intensification of afterburning of the products of jet fuel in the atmospheric oxygen. EFFECT: enhanced efficiency of missile carrier. 2 dwg
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