Bruce Banks - Academia.edu (original) (raw)
I have a background in atomic oxygen durability of spacecraft materials, ion beam sputtering, and electric propulsion.
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Surfaces on the leading edge of spacecraft in low Earth orbit (e.g., surfaces facing the velocity... more Surfaces on the leading edge of spacecraft in low Earth orbit (e.g., surfaces facing the velocity direction), such as on the International Space Station, are subject to atomic oxygen attack, and certain materials are susceptible to erosion. Therefore, ground-based laboratory testing of the atomic oxygen durability of spacecraft materials is necessary for durability assessment when flight data are not available. For accurate space simulation, the facility is commonly calibrated on the basis of the mass loss of Kapton (DuPont, Wilmington, DE) as a control sample for effective fluence determination. This is because Kapton has a well-characterized atomic oxygen erosion yield (Ey, in cubic centimeters per atom) in the low Earth orbit (LEO) environment.
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Triennial meeting (12th), Lyon, …, 1999
... Author: Rutledge, Sharon K.; Banks, Bruce A.; Chilchernea, Virgil A. Title Article/Chapter: &... more ... Author: Rutledge, Sharon K.; Banks, Bruce A.; Chilchernea, Virgil A. Title Article/Chapter: "Recovery of a charred painting using atomic oxygen ... atomic oxygen treatment does appear to be a technique with great potential for allowing very charred, previously unrestorable art to be ...
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AIP Conference Proceedings, 2009
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45th AIAA Aerospace Sciences Meeting and Exhibit, 2007
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A numerical procedure is presented to calculate transmittance degradation caused by contaminant f... more A numerical procedure is presented to calculate transmittance degradation caused by contaminant films on spacecraft surfaces produced through the interaction of orbital atomic oxygen (AO) with volatile silicones and hydrocarbons from spacecraft components. In the model, contaminant accretion is dependent on the adsorption of species, depletion reactions due to gas-surface collisions, desorption, and surface reactions between AO and silicon producing
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Protection of Space Materials from the Space Environment, 2001
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Page 1. Bruce A. Banks and Kim K. de Groh Lewis Research Center, Cleveland, Ohio Thomas J. Stuebe... more Page 1. Bruce A. Banks and Kim K. de Groh Lewis Research Center, Cleveland, Ohio Thomas J. Stueber and Edward A. Sechkar NYMA, Inc., Brook Park, Ohio Rachelle L. Hall Ohio Aerospace Institute, Cleveland, Ohio Ground Laboratory Soft X-Ray Durability ...
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AIP Conference Proceedings, 2009
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Journal of the American Institute For Conservation, Jul 18, 2013
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Surfaces on the leading edge of spacecraft in low Earth orbit (e.g., surfaces facing the velocity... more Surfaces on the leading edge of spacecraft in low Earth orbit (e.g., surfaces facing the velocity direction), such as on the International Space Station, are subject to atomic oxygen attack, and certain materials are susceptible to erosion. Therefore, ground-based laboratory testing of the atomic oxygen durability of spacecraft materials is necessary for durability assessment when flight data are not available. For accurate space simulation, the facility is commonly calibrated on the basis of the mass loss of Kapton (DuPont, Wilmington, DE) as a control sample for effective fluence determination. This is because Kapton has a well-characterized atomic oxygen erosion yield (Ey, in cubic centimeters per atom) in the low Earth orbit (LEO) environment.
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Triennial meeting (12th), Lyon, …, 1999
... Author: Rutledge, Sharon K.; Banks, Bruce A.; Chilchernea, Virgil A. Title Article/Chapter: &... more ... Author: Rutledge, Sharon K.; Banks, Bruce A.; Chilchernea, Virgil A. Title Article/Chapter: "Recovery of a charred painting using atomic oxygen ... atomic oxygen treatment does appear to be a technique with great potential for allowing very charred, previously unrestorable art to be ...
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AIP Conference Proceedings, 2009
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45th AIAA Aerospace Sciences Meeting and Exhibit, 2007
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A numerical procedure is presented to calculate transmittance degradation caused by contaminant f... more A numerical procedure is presented to calculate transmittance degradation caused by contaminant films on spacecraft surfaces produced through the interaction of orbital atomic oxygen (AO) with volatile silicones and hydrocarbons from spacecraft components. In the model, contaminant accretion is dependent on the adsorption of species, depletion reactions due to gas-surface collisions, desorption, and surface reactions between AO and silicon producing
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Protection of Space Materials from the Space Environment, 2001
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Page 1. Bruce A. Banks and Kim K. de Groh Lewis Research Center, Cleveland, Ohio Thomas J. Stuebe... more Page 1. Bruce A. Banks and Kim K. de Groh Lewis Research Center, Cleveland, Ohio Thomas J. Stueber and Edward A. Sechkar NYMA, Inc., Brook Park, Ohio Rachelle L. Hall Ohio Aerospace Institute, Cleveland, Ohio Ground Laboratory Soft X-Ray Durability ...
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Bookmarks Related papers MentionsView impact
AIP Conference Proceedings, 2009
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Journal of the American Institute For Conservation, Jul 18, 2013
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