FIELD: astronautics.
SUBSTANCE: invention relates to space engineering, particularly, to realization of multi-sectional designs of spacecrafts. Disclosed method of multisection structures consists in removal of main links, turn of sections, removal of additional links after turning and fixing section in final position. Additional links are provided by a retainer made in the form of a spring-loaded lever in contact with the support elements of the sections and resting on the solar battery frame during turning. Support elements of sections contain axes. Lever is fixed movably on the axis of the support element of the middle section. Lever arms are terminated by oppositely directed hooks until lateral sections are engaged with axes of support elements. One end of the spring is connected to the support element of the middle section, and the other one - to the arm of the lever.
EFFECT: enabling the design simplification.
1 cl, 7 dwg
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