Abstract: A space-stable thin film composite coating is provided that exhibits high IR emittance properties similar to OSR mirrors, and which is thin enough to be applied to a flexible substrate. The composite coating can include hundreds of alternating layers of aluminum oxide and silicon dioxide vacuum deposited to individual layer thickness of about 150 Angstroms and 50 Angstroms, respectively. The composite coating can be attached to substrates having complex geometries, for example, at various points during integration and production of hardware. The thin film can increase thermal design efficiency, reduce radiator mass and costs, and reduce production time-frames by eliminating the complexity of OSR mirror bonding.

Abstract: A method of making a multi-layer coating on a substrate is provided and involves applying a mirror coating to a substrate then spraying a silicate topcoat onto the mirror coating. Applying the mirror coating can involve applying a reflective material to the substrate to form a reflective layer and applying an oxide layer to the reflective layer to form the mirror coating. The oxide layer can be made of one or more oxide layers, and each of the one or more oxide layers can include aluminum oxide, silicon oxide, or a combination thereof. The multi-layer coating provides increased IR emittance and decreased solar absorptance relative to conventional thermal control coatings.

Abstract: A method of making a thermal control coating is provided. A primer layer can be applied to a substrate to form an exposed surface. The primer layer can include an epoxy binder and a silica filler. The exposed surface can be treated with an oxygen plasma to form a treated surface. A silicate-based thermal control coating can be applied to the treated surface, for example, by spraying, to form a thermal control coating on the substrate. Spacecraft and spacecraft hardware components coated with the thermal control coating, are also provided.

Abstract: A method is provided to form a dust mitigation coating that also mitigates or repels water, ice, and other liquids. Techniques to coat the surfaces of equipment and items with these dust, liquid, and ice mitigation coatings, minimize or eliminate mission problems caused by dust, liquid, or ice accumulation, particularly in outer space or on another planetary body or moon. Further, the dust mitigation coatings exhibit a Lotus-like effect, making the coated surfaces ultra-hydrophobic. The present invention is also directed to techniques for improving the functioning of terrestrial-based equipment and systems where dust, liquid, or ice accumulation is a problem, such as in hospitals and other health contexts, to prevent contamination.

Abstract: A laminate has a composite coating on a reflective substrate. The composite coating includes a stack of metal oxide trilayers on the substrate, where each metal oxide trilayer includes a layer of aluminum oxide; a layer of silicon oxide; and a layer of indium tin oxide. The composite coating also includes a stack of metal oxide bilayers on the metal oxide trilayer stack, each metal oxide bilayer including a layer of aluminum oxide and a layer of silicon oxide.

Abstract: A laminate has a composite coating on a substrate. The substrate is a polymeric substrate with a surface resistivity of 4×102 to 1×108?/?; or a textured substrate with surface features which are 100 nm to 10 microns high. The composite coating comprising a tie layer of a nickel-chromium alloy; a layer of a reflective metal; a layer of aluminum oxide; a layer of silicon oxide; and optionally a layer of indium tin oxide. The laminate has a solar absorbance at a wavelength of 0.25 microns to 2.5 microns of between 0.07 and 0.7; and the laminate has an IR emittance of 0.1 to 0.8. Solar absorbance and IR emittance of the laminate may be independently to control the ratio of solar absorbance to IR emittance. Solar absorbance may be adjusted by changing the surface resistance or degree of texturing on the substrate. IR emittance may be adjusted by changing oxide film thickness.

Abstract: In one embodiment, a system includes a first cold noise source, a first radiometer receiver, and a first detector. The first cold noise source generates a first thermal radiation signal having a first carrier frequency band. The first thermal radiation signal carries a first information signal. The first cold noise source also transmits the first thermal radiation signal through a first antenna. The first radiometer receiver receives the first thermal radiation signal through a second antenna, and the first detector extracts the first information signal from the first thermal radiation signal.

Abstract: In one embodiment, a system includes a first cold noise source, a first radiometer receiver, and a first detector. The first cold noise source generates a first thermal radiation signal having a first carrier frequency band. The first thermal radiation signal carries a first information signal. The first cold noise source also transmits the first thermal radiation signal through a first antenna. The first radiometer receiver receives the first thermal radiation signal through a second antenna, and the first detector extracts the first information signal from the first thermal radiation signal.

Abstract: A coating for wall construction is provided whereby a level 5 finish may be obtained without the need for a finishing coat or final skim coat. The coating may be applied to drywall elements prior to installation and is compatible with jointing materials such that a substantially homogeneous surface may be obtained after the drywall elements are assembled with jointing material and the jointing material is dried. The coating formulation includes a noncellulosic thickener, a binder, a mineral filler and water. A method for the construction of interior walls and a construction assembly for interior walls is further provided.

Abstract: Coating and jointing material systems for wall construction are provided. The coating is applied to drywall elements prior to installation and is compatible with the jointing materials such that a substantially homogeneous surface may be obtained after the drywall elements are assembled with jointing material and the jointing material is dried. Methods for the construction of interior walls and interior construction systems are provided.

Abstract: Coating and jointing material systems for wall construction are provided. The coating is applied to drywall elements prior to installation and is compatible with the jointing materials such that a substantially homogeneous surface may be obtained after the drywall elements are assembled with jointing material and the jointing material is dried. Methods for the construction of interior walls and interior construction systems are provided.

Abstract: A coating for wall construction is provided whereby a level 5 finish may be obtained without the need for a finishing coat or final skim coat. The coating may be applied to drywall elements prior to installation and is compatible with jointing materials such that a substantially homogeneous surface may be obtained after the drywall elements are assembled with jointing material and the jointing material is dried. The coating formulation includes a noncellulosic thickener, a binder, a mineral filler and water. A method for the construction of interior walls and a construction assembly for interior walls is further provided.