FIELD: transport.
SUBSTANCE: invention relates to space engineering, particularly, to spacecraft separation devices. Proposed system comprises split retainer arranged between bearing structure with hole and spacecraft with hole with ledges for locking of the thrust. Besides, it has mechanical locks with rod and washer and hole displaced relative to rod axis. Locking link retains the link with recess of pivot pin.
EFFECT: reliable separation of payload.
4 dwg
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Authors
Dates
2015-10-10—Published
2014-09-03—Filed