A method for attaching a heat-emitting device and a capillary heat pipe to a panel of a spacecraft wall is disclosed including the steps of: a) positioning a capillary heat pipe on a portion of the panel; attaching female attachment bodies to the panel, the female attachment bodies protruding relative to the capillary heat pipe; c) placing a thermally-conductive and self-curing paste over a portion of the capillary heat pipe or over a heat-emitting device; d) placing a heat-emitting device on the thermally-conductive and self-curing paste and on the female attachment bodies, said heat-emitting device bearing against and being in direct contact with the female attachment bodies, and e) attaching the heat-emitting device and said capillary heat pipe to the panel by attaching male attachment members to the female attachment bodies.
PROCÉDÉ DE FIXATION D'UN ÉQUIPEMENT DISSIPATIF, MUR DE VÉHICULE SPATIAL ET VÉHICULE SPATIAL
METHOD FOR ATTACHING A HEAT-DISSIPATING PIECE OF EQUIPMENT, SPACECRAFT WALL AND SPACECRAFT
VERFAHREN ZUR BEFESTIGUNG EINES WÄRMEABFÜHRENDEN TEILS EINER AUSRÜSTUNG, RAUMFAHRZEUGWAND UND RAUMFAHRZEUG
2022-04-20
Patent
Electronic Resource
French
IPC: | B64G Raumfahrt , COSMONAUTICS |
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