FIELD: astronautics.
SUBSTANCE: invention relates to protection of space vehicles (SV) against collision with other orbital bodies, in particular, space debris. Method consists in pulse repulsion and separation of cable connected modules forming SV, to their exit from dangerous zone. After cable deployment and fixation of its length modules ligament is switched to associated pendulum motion mode. At its end is mutual approach modules by cable is performed, and further docking. Cable supply and pulling are made with constant tension force, overload of which is proportional to modules repulsion velocity pulse value.
EFFECT: simple technique, facilities and control algorithms over such SV evasive action.
1 cl, 4 dwg
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Authors
Dates
2016-06-10—Published
2015-01-26—Filed