Method for attaching a heat-emitting device, spacecraft wall and spacecraft

A method for attaching a heat-emitting device and a capillary heat pipe to a panel of a spacecraft wall, comprising:

• a) arranging at least one capillary heat pipe on at least a portion of the panel;
• b) attaching female attachment bodies to the panel, the female attachment bodies protruding from said at least one capillary heat pipe;
• c) placing a thermally-conductive and self-curing paste on at least a portion of the at least one capillary heat pipe or on at least one heat-emitting device,
• d) placing the at least one heat-emitting device on the thermally-conductive and self-curing paste and on the female attachment bodies, said heat-emitting device bearing against the female attachment bodies, said heat-emitting device is in direct contact with the female attachment bodies, and
• e) attaching the heat-emitting device and said at least one capillary heat pipe to the panel by attaching male attachment members to the female attachment bodies.