A multi-layer insulation (MLI) blanket with enhanced contamination inhibiting properties and a method for inhibiting the formation of organic residues on the outer surface of a MLI blanket are provided. In one embodiment, a MLI blanket (10) attachable to a spacecraft or other structure includes a pl
A multi-layer insulation (MLI) blanket with enhanced contamination inhibiting properties and a method for inhibiting the formation of organic residues on the outer surface of a MLI blanket are provided. In one embodiment, a MLI blanket (10) attachable to a spacecraft or other structure includes a plurality of metallized layers (20, 30, 40, 50) separated by mesh layers (60, 62, 64). An anti-contamination coating (80) comprised of a photocatalytic material is disposed between a high emittance layer (70) that overlies the outer surface (20A) of the outer metallized layer (20) and an outer electrically conductive layer (90). When exposed to ultraviolet or near-ultraviolet radiation components present in solar radiation, the anti-contamination coating (80) catalyzes the breakdown of organic residues on the outer surface of the MLI blanket (10) thereby maintaining the reflective properties of the MLI blanket (10) and ensuring that solar absorptance of the MLI blanket (10) is maintained at or below an acceptable threshold level.
대표청구항▼
What is claimed is: 1. A multi-layer insulation blanket providing thermal protection to a spacecraft portion comprising: a portion of the spacecraft on which thermal protection is desirable; and a multi-layer insulation blanket attachable on the portion of the spacecraft to provide thermal protecti
What is claimed is: 1. A multi-layer insulation blanket providing thermal protection to a spacecraft portion comprising: a portion of the spacecraft on which thermal protection is desirable; and a multi-layer insulation blanket attachable on the portion of the spacecraft to provide thermal protection to the portion of the spacecraft, said multi-layer insulation blanket including: an outer sheet of thermally insulative plastic material, said outer sheet having a reflective surface on a side of said outer sheet of thermally insulative plastic material facing space when said multi-layer insulation blanket is attached to the spacecraft; at least one inner sheet of thermally insulative plastic material between said outer sheet of thermally insulative plastic material and the spacecraft when said multi-layer insulation blanket is attached to the spacecraft; a coating of anti-contaminant material overlying said reflective surface of said outer sheet of thermally insulative plastic material, said coating of anti-contaminant material being effective to induce the breakdown of organic residues on said outer surface of said outer sheet of thermally insulative plastic material in the presence of solar radiation, said coating of anti-contaminant material having a thickness no greater than 200 nanometers; and an outermost electrically conductive layer overlying said coating of anti-contaminant material. 2. The multi-layer insulation blanket of claim 1 wherein said outer sheet of thermally insulative plastic material comprises metallized polyimide material or metallized polyester material. 3. The multi-layer insulation blanket of claim 1 wherein said at least one inner sheet of thermally insulative plastic material comprises polyimide material or polyester material. 4. The multi-layer insulation blanket of claim 1 wherein said at least one inner sheet of thermally insulative plastic material is metallized. 5. The multi-layer insulation blanket of claim 1 wherein said outer sheet of thermally insulative plastic material and said at least one inner sheet of thermally insulative plastic material are coextensive with one another. 6. The multi-layer insulation blanket of claim 1 wherein said anti-contaminant material comprises a photocatalytic material. 7. The multi-layer insulation blanket of claim 6 wherein said photocatalytic material comprises a photoactive transition metal oxide. 8. The multi-layer insulation blanket of claim 7 wherein said photoactive transition metal oxide is selected from the group consisting of TiO2, ZnO, WO3, CaTiO3, SnO2, MoO3, NbO5, Fe2O3, Ta2O5, and TiX(Zr1-X)O2, where X has a value of between 0 and 1. 9. The multi-layer insulation blanket of claim 1 further comprising at least one layer of lightweight spacing material disposed between said outer sheet of thermally insulative plastic material and said at least one inner sheet of thermally insulative plastic material. 10. The multi-layer insulation blanket of claim 9 wherein said lightweight spacing material comprises nylon mesh or glass fiber mesh. 11. The multi-layer insulation blanket of claim 1 further comprising a high emittance layer between said reflective surface and said coating of anti-contaminant material. 12. The multi-layer insulation blanket of claim 11 wherein said high emittance layer comprises a material selected from the group consisting of glass, quartz, silicon nitride, and silicon oxy-nitride. 13. The multi-layer insulation blanket of claim 1 wherein said electrically conductive layer comprises one of indium tin oxide and indium oxide. 14. A multi-layer insulation blanket attachable on a structure intended for use in vacuum conditions, said multi-layer insulation blanket comprising: an outer sheet of thermally insulative plastic material, said outer sheet having a reflective surface on at least a first side thereof facing away from said structure when said multi-layer insulation blanket is attached to the structure; at least one inner sheet of thermally insulative plastic material between said outer sheet and the structure when said multi-layer insulation blanket is attached to the structure; a high emittance layer overlying said reflective surface of said outer sheet of thermally insulative plastic material; a coating of photocatalytic material overlying said high emittance layer, wherein said coating of photocatalytic material catalyzes the breakdown of organic residues on said outer surface of said outer sheet of thermally insulative plastic material when exposed to at least one of ultraviolet and near-ultraviolet radiation, and wherein said coating of photocatalytic material has a thickness no greater than 200 nanometers; and an outermost electrically conductive layer overlying said coating of photocatalytic material. 15. The multi-layer insulation blanket of claim 14 wherein said outer sheet of thermally insulative plastic material comprises metallized polyimide material or metallized polyester material. 16. The multi-layer insulation blanket of claim 14 wherein said at least one inner sheet of thermally insulative plastic material comprises polyimide material or polyester material. 17. The multi-layer insulation blanket of claim 14 wherein said at least one inner sheet of thermally insulative plastic material is metallized. 18. The multi-layer insulation blanket of claim 14 wherein said outer sheet of thermally insulative plastic material and said at least one inner sheet of thermally insulative plastic material are coextensive with one another. 19. The multi-layer insulation blanket of claim 14 wherein said photocatalytic material comprises a photoactive transition metal oxide. 20. The multi-layer insulation blanket of claim 19 wherein said photoactive transition metal oxide is selected from the group consisting of TiO2, ZnO, WO3, CaTiO3, SnO2, MoO3, NbO5, Fe2O3, Ta2O5, and TiX(Zr1-X)O2, where X has a value of between 0 and 1. 21. The multi-layer insulation blanket of claim 14 further comprising at least one layer of lightweight spacing material disposed between said outer sheet of thermally insulative plastic material and said at least one inner sheet of thermally insulative plastic material. 22. The multi-layer insulation blanket of claim 21 wherein said lightweight spacing material comprises nylon mesh or glass fiber mesh. 23. The multi-layer insulation blanket of claim 14 wherein said high emittance layer comprises a material selected from the group consisting of glass, quartz, silicon nitride, and silicon oxy-nitride. 24. The multi-layer insulation blanket of claim 14 wherein said electrically conductive layer comprises one of indium tin oxide and indium oxide. 25. The multi-layer insulation blanket of claim 14 wherein the structure comprises a spacecraft.
Gonczy John D. (Oak Lawn IL) Niemann Ralph C. (Downers Grove IL) Boroski William N. (Aurora IL), Multilayer insulation blanket, fabricating apparatus and method.
Lepore ; Jr. Albert (Upper Holland PA) Wong Hamilton (Pennington NJ) Marr Susan L. (Northampton Township ; Bucks County PA) Amore Leo J. (Phoenixville PA), RF-transparent antenna sunshield membrane.
Ross Barry S. (Manhattan Beach CA) Reynolds Robert L. (Los Angeles CA) Vanbebber Glen A. (Torrance CA) White Daniel A. (Manhattan Beach CA), Spacecraft protective blanket.
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