Abstract: A gas turbine engine article includes a silicon-containing ceramic wall that has an external combustion gaspath side and an internal side that borders a cooling air cavity. The external combustion gaspath side has an associated combustion gas flow direction there along. An array of cooling holes extends through the silicon-containing ceramic wall and connects the internal side with the external combustion gaspath side. The cooling holes are oriented to discharge cooling air to the external gaspath side in a direction counter to the combustion gas flow direction.

Abstract: A method of mounting and interconnecting solar cells to form a solar cell array particularly suited to space applications. In the present invention, the solar cells, which are already silver plated on the underside, are diffusion welded to a suitably plated polymide film substrate. The attachment area and current conductor patterns are provided in the plating on the substrate and electrical connection of the solar cells is accomplished by soldering or diffusion welding directly to the plated pattern on the substrate.