SPACECRAFT DOCKING DEVICE Russian patent published in 2013 - IPC B64G1/64 F42B15/36 

Abstract RU 2490183 C1

FIELD: transport.

SUBSTANCE: invention relates to space engineering. Spacecraft docking device comprise active unit with docking mechanism arranged at its center and passive unit with mate intake cone terminated in mount. Said intake cone is composed by nozzle of sustainer rocket engine of separable last stage of spaceship. Docking mechanism is composed of telescoping bars with free end furnished with spring-loaded parasol-shaped lugs arranged to unlock and lock.

EFFECT: simplified docking.

4 dwg

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RU 2 490 183 C1

Authors

Trushljakov Valerij Ivanovich

Jutkin Evgenij Alekseevich

Tjutebaev Talgat Kenzhebaevich

Shatrov Jakov Timofeevich

Makarov Jurij Nikolaevich

Dates

2013-08-20Published

2012-03-07Filed