FIELD: transport.
SUBSTANCE: invention relates to aerospace engineering, particularly, to means for placing spaceships in orbit. Proposed system comprises carrier rocket with bearing compartment at carrier rocket final stage to allow coupling carrier rocket to nose cone of diameters exceeding that of rocket final stage, and spacecraft. Rocker carrier final stage and bearing compartment comprises common structural frame composed of two fixed and two detachable sectors interconnected by fasteners. Detachable sectors are located diametrically opposite. To fit locks in place for separation of nose cone from rocket carrier final stage recesses are made in both sectors.
EFFECT: simplified attachment of nose cones to carrier rockets.
4 dwg
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Authors
Dates
2013-06-27—Published
2011-12-28—Filed