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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Authors
Dates
2013-08-20—Published
2012-03-07—Filed