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
THERMISCHES KONTROLLBAND, SYSTEM UND VERFAHREN FÜR EINE RAUMFAHRZEUGSTRUKTUR
RUBAN DE COMMANDE THERMIQUE, SYSTÈME ET PROCÉDÉ POUR UNE STRUCTURE DE VÉHICULE SPATIAL
2022-05-04
Patent
Electronic Resource
English
THERMAL CONTROL TAPE, THERMAL CONTROL TAPE SYSTEM, AND METHOD FOR SPACECRAFT STRUCTURE
European Patent Office | 2019
|THERMAL CONTROL TAPE, SYSTEM, AND METHOD FOR A SPACECRAFT STRUCTURE
European Patent Office | 2019
|NTIS | 2001
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