Cooled insulation surface temperature control system

Aeronautics and astronautics – Spacecraft – Spacecraft formation – orbit – or interplanetary path

Reexamination Certificate

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Reexamination Certificate

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07055781

ABSTRACT:
An apparatus and method for surface temperature control is provided. Surface temperature control is achieved by flowing coolant in and then out of a low strength porous layer attached to a structural plenum. A semi-permeable layer may be attached to the outer surface of the porous layer to prevent erosion of the porous layer and to facilitate surface film cooling.

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