FIELD: space flights. SUBSTANCE: device has elastic members 3, located between a base (vibration source) 1 and equipment 2. Central part of the elastic members is made as zigzag-shaped bent in inter-perpendicular planes pipes 4, passed between elastic stops-deflectors 12. Members 3 are made as coaxial trunks, that provide high current electric power feeding of equipment 2 by central cable wire and feeding and removal of heat-carrier by the first coaxial pipeline, embracing the wire and lower current feeding - by conductive members, applied on inner surface of the trunk shell. In the case, a damping member, for example, in the form of pressed metal wire, is placed between the shell and cylindrical wall of the heat pipeline. EFFECT: device, using minimum additional spacecraft means, provides reliable HF-vibroinsulation of the equipment. 2 cl, 3 dwg
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Authors
Dates
1994-08-15—Published
1990-06-11—Filed