(GB2323473-A)      The solar module has a number of individual solar cells (3) positioned in a regular array on a large surface area carrier (2), each provided with a glass cover having a transparent conductive coating. An electrically insulating material is inserted between the glass covers of the adjacent solar cells, with the conductive coatings applied to the glass covers electrically connected at the corners of the latter via coupling plates secured to the coatings via a conductive adhesive.    USE -   For space satellite solar generator.    ADVANTAGE -   Provides stable electrical connections between solar cells with minimum risk of short-circuits.    (JP11017205-A)      The solar module has a number of individual solar cells (3) positioned in a regular array on a large surface area carrier (2), each provided with a glass cover having a transparent conductive coating. An electrically insulating material is inserted between the glass covers of the adjacent solar cells, with the conductive coatings applied to the glass covers electrically connected at the corners of the latter via coupling plates secured to the coatings via a conductive adhesive.    USE -   For space satellite solar generator.    ADVANTAGE -   Provides stable electrical connections between solar cells with minimum risk of short-circuits.    (US5942046-A)      The solar module has a number of individual solar cells (3) positioned in a regular array on a large surface area carrier (2), each provided with a glass cover having a transparent conductive coating. An electrically insulating material is inserted between the glass covers of the adjacent solar cells, with the conductive coatings applied to the glass covers electrically connected at the corners of the latter via coupling plates secured to the coatings via a conductive adhesive.    USE -   For space satellite solar generator.    ADVANTAGE -   Provides stable electrical connections between solar cells with minimum risk of short-circuits.    (JP2984248-B2)      The solar module has a number of individual solar cells (3) positioned in a regular array on a large surface area carrier (2), each provided with a glass cover having a transparent conductive coating. An electrically insulating material is inserted between the glass covers of the adjacent solar cells, with the conductive coatings applied to the glass covers electrically connected at the corners of the latter via coupling plates secured to the coatings via a conductive adhesive.    USE -   For space satellite solar generator.    ADVANTAGE -   Provides stable electrical connections between solar cells with minimum risk of short-circuits.