초록 ▼

By the installation of elastic elements between a rocket and a retaining sleeve (or, respectively, a retaining sleeve and a launching device, or within a launching device), peak loads are reduced and breakage of a connecting member or, respectively, of the parts of the retaining sleeve corresponding

By the installation of elastic elements between a rocket and a retaining sleeve (or, respectively, a retaining sleeve and a launching device, or within a launching device), peak loads are reduced and breakage of a connecting member or, respectively, of the parts of the retaining sleeve corresponding to this connecting member is avoided.

대표청구항 ▼

A rocket retainer in a launching device for at least one rocket inserted in a retaining sleeve connectible to the launching device wherein the attachment of the rocket in the retaining sleeve takes place via a connecting member, the connecting member exhibiting a conical end which can be expanded an

A rocket retainer in a launching device for at least one rocket inserted in a retaining sleeve connectible to the launching device wherein the attachment of the rocket in the retaining sleeve takes place via a connecting member, the connecting member exhibiting a conical end which can be expanded and positioned by means of a displacement pin at a detachable sealing lid of the retaining sleeve, the expanded connecting member engaging at the retaining sleeve, and the connection of the rocket with the retaining sleeve being releasable by removal of the displacement pin, characterized in that at least one damping elastic element is provided between the rocket and the launching device in such a way that, upon an axial movement of the rocket, deformation of an elastic element takes place.