A thermal control tape for providing thermal control of a spacecraft structure, to which the thermal control tape is applied is provided. The thermal control tape has a filled silicone resin layer having a first side and a second side. The filled silicone resin layer has a silicone resin material filled with a white inorganic filler material. The tape further has a silicone pressure sensitive adhesive (PSA) layer having a first side and a second side, the first side of the silicone PSA layer attached to the second side of the filled silicone resin layer. The filled silicone resin layer and the silicone PSA layer form the thermal control tape, with the second side of the silicone PSA layer configured for attachment to at least one surface of the spacecraft structure of a spacecraft, to provide thermal control of the spacecraft structure, by radiating heat away from the spacecraft structure.
THERMAL CONTROL TAPE, SYSTEM, AND METHOD FOR A SPACECRAFT STRUCTURE
2019-05-23
Patent
Electronic Resource
English
IPC: | B64G Raumfahrt , COSMONAUTICS / B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse / C09J ADHESIVES , Klebstoffe / F28F Einzelheiten von Wärmetauschern oder Wärmeübertragungsvorrichtungen für allgemeine Verwendung , DETAILS OF HEAT-EXCHANGE OR HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION / H05F STATIC ELECTRICITY , Statische Elektrizität |
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