Abstract A method and apparatus for grounding multi-layer insulations (MLI) by electric contact, of either of each layer with the other or of all the layers with the underlying structure by means of one or more points of attachment of mechanical type. This makes it possible to simplify the construction procedure and increase the reliability. This method is essentially carried out in the following manner: The layers (FIG. 1) which form the multi-layer insulations (6), (7) (8) are metalized on both faces and have holes (9) which are also metalized. All layers are contacted with each other and with a part of the attachment system (3) which is also electrically conductive. The other part of the attachment system (2) is positioned on the structure (1) in such a manner as to permit the passage of electric charges. By contacting the two parts of the attachment system (2) (3), the multi-layer insulation is grounded with the structure. The invention lies within the technical field of passive thermal protections, especially for space structures (space apparatus and systems etc.). The object of the invention is to permit the removal of electric charges on multi-layer insulations.
A multi-layer insulation for the passive thermal control of satellites or space structures comprising outer, intermediate and inner superposed layers, the outer layer of the multi-layer insulation (7) being electrically conductive on its two faces (13) (14), said two faces of said outer layer being electrically connected by the presence of holes (9) through said outer layer the walls of which are electrically conductive (11); both faces of the other layers (6) (8) being electrically conductive, said both faces of each other layer being electrically connected by the presence of holes (9) the walls of which are conductive; an underlying structure, means for attaching the multi-layer insulation (12) to the underlying structure (1) including a hook and pile fastener (2 and 3) of electrically conductive material; one part of the hook and pile fastener being electrically conductively attached to the multi-layer insulation (12) and the other part being electrically conductively attached to the underlying structure (1).
Claim 2
Dependent Claim
156 words
A multi-layer insulation for the passive thermal control of satellites or space structures comprising outer, intermediate and inner superposed layers, the outer layer of the multi-layer insulation (7) being electrically conductive on its two faces (13) (14), said two faces of said outer layer being electrically connected by the presence of holes (9) through said outer layer the walls of which are electrically conductive (11); both faces of the other layers (6) (8) being electrically conductive, said both faces of each other layer being electrically connected by the presence of holes (9) the walls of which are conductive; an underlying structure, means for attaching the multi-layer insulation (12) to the underlying structure (1) including a hook and pile fastener (2 and 3) of electrically conductive material; one part of the hook and pile fastener being electrically conductively attached to the multi-layer insulation (12) and the other part being electrically conductively attached to the underlying structure (1).
Claim 3
Dependent Claim
86 words
The multi-layer insulation of claim 1, characterized by the fact that the inner layer (8) is electrically conductive only on one of its surfaces and that on each layer (6), (7), (8) of the multi-layer insulation (12) there extending through said slit cuts, and means (18) for holding said metal element in such a manner as to place the layers of the multi-layer insulation (6), (7), (8) and the hook part (2) or pile part (3) of the attachment system in contact with said metallic element.