TRANSPORT-LAUNCHING MODULE Russian patent published in 2005 - IPC

FIELD: rocketry, in particular, launchers of surface ships and submarines.

SUBSTANCE: the transport-launching module has a sealed casing in the form of a cup with the front and rear covers with a seal. A rocket with a nose cone is installed inside the cup. The rocket nose cone partially projects from the cup, and in the assembled state of the transport-launching module serves at the same time as the front cover of the transport-launching module cover. The transport-launching module is provided with a changeable ring component, whose one end face is conjugate to the respective end face of the cup. Longitudinally positioned threaded members (for example, bolts) are passed through the changeable ring component, with the aid of them the changeable ring component is connected to the cup. BY means of longitudinally positioned break-off components made in the form, for example, of explosive bolts, as well as of radially positioned break-off components made, for example, in the form of explosive bolts the changeable ring component is fastened to the rocket nose cone. Inside the transport-launching module provision is made for an obturator, which is positioned in the bottom (tail) section of the rocket. The cup is made with an inner smooth cylindrical surface. Detachable means for creation of a behind-rocket volume of the preset value are installed on the rear cover with the id of brackets.

EFFECT: reduced thermoerrosion effect on the casing of the transport-launching module at a launch of the rocket, which makes it re-usable.

7 cl, 6 dwg