SPACECRAFT MATING UNIT Russian patent published in 2002 - IPC

Abstract RU 2195417 C2

FIELD: high-precision mating of space objects, flying vehicles and submarine vessels. SUBSTANCE: device includes mating unit which is tightly connected with rigid case through bellows-type transient compartment strengthened by load-bearing framework made from rod members. Load-bearing framework is mounted coaxially relative to transient compartment between case and mating unit for spatial orientation and compensation of impact in mating. Load-bearing framework is made in form of drive six- articulation kinematic joint. EFFECT: enhanced reliability of mating of space object (orbital station) with spacecraft; extended functional capabilities of space object. 2 cl, 2 dwg

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RU 2 195 417 C2

Authors

Sajapin S.N.

Sinev A.V.

Dates

2002-12-27Published

2000-09-13Filed