FIELD: space technology. SUBSTANCE: bar deployment mechanism has base 1, axle 3 with fixed bar, main drive 4 and alternate drive 5 in the form of torsional spring. Main drive 5 is engageable with the longer arm of rocker 10 and alternate drive 5 - with the shorter arm of rocker 10. The ratio between the lengths of rocker arms is determined by the inequality presented in the text of the claimed invention. EFFECT: higher operating reliability. 1 dwg
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