SPACECRAFT Russian patent published in 2004 - IPC

Abstract RU 2231484 C2

FIELD: space engineering; designing spacecraft provided with radar and optical systems.

SUBSTANCE: proposed spacecraft includes case and solar battery panels. Mounted in between case and each solar battery panel are multi-member folding braces which are articulated on case at one end and on solar battery panels at other end at points selected on the condition of equality of sum of inertial forces of cantilever and root parts of panels at transversal oscillations; longitudinal axes of braces pass through center of mass of spacecraft.

EFFECT: reduction of time of transient processes; extended time for performing functional mission of spacecraft.

5 dwg

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RU 2 231 484 C2

Authors

Dmitriev V.V.

Abramov B.A.

Kislinskij G.G.

Filippov Ju.I.

Dates

2004-06-27—Published

2002-06-18—Filed