A document discusses a zeolite-based sprayable molecular adsorber coating that has been developed to alleviate the size and weight issues of current ceramic puck-based technology, while providing a configuration that more projects can use to protect against degradation from outgassed materials within a spacecraft, particularly contamination-sensitive instruments. This coating system demonstrates five times the adsorption capacity of previously developed adsorber coating slurries. The molecular adsorber formulation was developed and refined, and a procedure for spray application was developed. Samples were spray-coated and tested for capacity, thermal optical/radiative properties, coating adhesion, and thermal cycling.
Work performed during this study indicates that the molecular adsorber formulation can be applied to aluminum, stainless steel, or other metal substrates that can accept silicatebased coatings. The coating can also function as a thermal-control coating. This adsorber will dramatically reduce the mass and volume restrictions, and is less expensive than the currently used molecular adsorber puck design.
This work was done by Sharon Straka, Wanda Peters, Mark Hasegawa, Randy Hedgeland, and John Petro of Goddard Space Flight Center and Kevin Novo-Gradac, Alfred Wong, Jack Triolo, and Cory Miller of SGT, Inc. GSC-16105-1