ROCKET-CARRIER MODULE Russian patent published in 2009 - IPC B64G1/22 F42B15/36 

FIELD: aerospace engineering.

SUBSTANCE: invention relates to the design of rocket-carrier "dry" modules, for examples, intertank and tail rocket stages that can accommodate instruments and hardware of various rocker-carrier systems (control systems, telemetry system, and the like). The proposed rocket-carrier module comprises a shell with hatch cut-out, cover attached along the said cut-out edges, crosswise load-bearing set representing, say, frames, and lengthwise load-bearing set representing, for example stringers. Aforesaid shell comprises brackets attached on the cut-out edges and to every adjustable-length fastening element screwed in aforesaid brackets. Structurally, aforesaid fastening element is made integral with the hatch cover to increase their load-bearing capacity.

EFFECT: lower weight, ease of manufacture, servicing and replacements.

6 cl, 4 dwg