Tecstar Power Systems, Inc.

Emcore Corporation

Mark DeWitt

James Patrick Hanley

Louis C Kilmer

Peng-Kuen Chiang

Eugene L Ralph

Norman L Beze

James R Walle

Ellen B Linder

An efficient method of interconnecting a solar cell having at least two front surface contacts with a diode mounted on a front surface of the solar cell includes the act of forming at least a first recess on a front surface of the solar cell. A first solar cell contact is formed on the front surface in the first recess. A second solar cell contact is formed on the front surface. At least a first bypass diode is positioned at least partly within the recess. The bypass diode has a first diode contact and a second diode contact. The first solar cell contact is interconnected with the first diode contact. The second solar cell contact is interconnected with the second diode contact.

Solar cell having a front-mounted bypass diode

A radiation tolerant solar cell array module which can be efficiently assembled into a larger solar panel to generate power for a spacecraft the module includes at least first and second single-crystal solar cells. The first and second solar cells have front sides and back sides. At least one of the solar cells has a shallow junction N on P structure. A first contact is formed on at least the back side of the first solar cell. A second contact formed on at least the back side of the second solar cell. A conductor is in electrical communication with the first contact and the second contact. A substantially transparent ceria-doped cover overlays at least a portion of each of the solar cells. The cover remains substantially transparent when exposed to an AM space radiation environment. A substantially transparent adhesive is situated between the cover and the solar cell portions. The adhesive remains substantially transparent when exposed to a space radiation environment.

Modular, glass covered solar cell array

A radiation tolerant solar cell array module which can be efficiently assembled into a larger solar panel to generate power for a spacecraft the module includes at least first and second single-crystal solar cells. The first and second solar cells have front sides and back sides. At least one of the solar cells has a shallow junction N on P structure. A first contact is formed on at least the back side of the first solar cell. A second contact formed on at least the back side of the second solar cell. A conductor is in electrical communication with the first contact and the second contact. A substantially transparent ceria-doped cover overlays at least a portion of each of the solar cells. The cover remains substantially transparent when exposed to an AM0 space radiation environment. A substantially transparent adhesive is situated between the cover and the solar cell portions. The adhesive remains substantially transparent when exposed to a space radiation environment.

Modular glass covered solar cell array

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Simi Valley, CA, United States of America

Mark DeWitt