초록 ▼

A subcaliber missile to be launched from a barrel, in order to serve as a carrier for satellite missiles of other ejectable bodies, has an envelope divided into two half-shells of tapering configuration which are articulated to the missile bottom and are held together by a missile head and by intern

A subcaliber missile to be launched from a barrel, in order to serve as a carrier for satellite missiles of other ejectable bodies, has an envelope divided into two half-shells of tapering configuration which are articulated to the missile bottom and are held together by a missile head and by internal partitions separating the ejectable bodies from one another. When the missile is in flight, the ejection of the head by the detonation of a charge exerts a backward reaction force upon the envelope, causing its load to move forward therein whereby the partitions are disengaged from the two half-shells and allow them to flip apart. The half-shells are provided with slots for a recessed tail-wing assembly and with back fins which, like the missile bottom, conform to the caliber of the barrel.

대표청구항 ▼

A carrier missile for ejectable bodies such as satellite missiles, mines and the like, adapted to be launched from a barrel, comprising a split missile envelope provided with a bottom and a head, designed to receive several aligned bodies, resting against partitions, which upon traverse of a certain

A carrier missile for ejectable bodies such as satellite missiles, mines and the like, adapted to be launched from a barrel, comprising a split missile envelope provided with a bottom and a head, designed to receive several aligned bodies, resting against partitions, which upon traverse of a certain flight path are released by the castoff of the missile head and the flipping-open of the missile envelope, said missile envelope being formed from half-shells and hingedly connected with the missile bottom, with a cylindrical interior and with an exterior converging conically toward the missile point, whose inner wall is provided with spaced-apart annular grooves receiving several partitions, individually supporting the bodies to be ejected, which in turn engage with their ends in the annular grooves in such a way that upon launching they clamp the half-shells of the missile envelope together but release them upon the ejection of the bodies.