The goals of the ICPMSE-7 meeting, as in the past years, are to facilitate exchanges between members of the various engineering disciplines involved in development of space materials, including such aspects as environmental hazards of Low Earth Orbit (LEO), Geostationary Earth Orbit (GEO) and Deep Space, ground-based qualification, and in-flight experiments and lessons learned from operational vehicles.The book continues to discuss topics started in the earlier publications and adds new data and results.The proceedings cover a range of inter-disciplinary topics concerning the protection of…mehr
The goals of the ICPMSE-7 meeting, as in the past years, are to facilitate exchanges between members of the various engineering disciplines involved in development of space materials, including such aspects as environmental hazards of Low Earth Orbit (LEO), Geostationary Earth Orbit (GEO) and Deep Space, ground-based qualification, and in-flight experiments and lessons learned from operational vehicles.The book continues to discuss topics started in the earlier publications and adds new data and results.The proceedings cover a range of inter-disciplinary topics concerning the protection of materials and structures in space and discussing the effects of the aggressive LEO as well as the GEO and Deep Space environments on materials and structures and the ways to predict and reduce these effects of short and long-term space missions.The book is targeting organizations and individuals involved with space material selction, their reliability and influence of space environmental effects on materials and structures.
Jacob I. Kleiman, Integrity Testing Laboratory Inc. Markham, ON, Canada
Inhaltsangabe
Introduction. Acknowledgements. Organization. Section A. Radiation effects of protons and electrons on Back-field silicon solar cells; Z. Hu, S. He, D. Yang . Solar array arcing in LEO: how much charge is discharged?; D.C. Ferguson, B.V. Vayner, J.T. Galofaro. Self-restoration as SEU protection mechanism for re-configurable on-board computing platform; L. Kirischian, et al . Synergistic effects of protons and electrons on radiation damage of methyl silicone rubber; L. Zhang et al . Influence of electron radiation on outgassing of spacecraft materials; R. H. Khassanchineet al . Effect of surface charging on the erosion rate of polyimide under 5 eV atomic oxygen beam exposure; M. Tagawa et al . Influence of space environment on spectral optical properties of thermal control coatings; V.M. Prosvirikov, et al. Mitigation of thruster plume-induced erosion of ISS sensitive hardware; C. Pankop, J. Alred, P. Boeder . Degradation of thermal control coatings under influence of proton irradiation; L.S. Noviko et al . Mitigation of damage to the international space station (ISS) from water dumps; W. Schmidl, J. Visentine, R. Mikatarian . Investigation of synergistic effects of proton and electron radiation on the dyeing of optical quartz glass; H. Liu et al . The role of "abnormal" electron fluxes with energy < 1 MeV in the surface charging dose of spacecraft; O.R. Grigoryan et al. Section B. Vacuum ultraviolet radiation effects on DC93-500 silicone film; J.A. Dever, B.A. Banks, L. Yan .Enhancement of atomic oxygen-induced erosion of spacecraft polymeric materials by simultaneous ultraviolet exposure; K. Yokota, N. Ohmae, M. Tagawa. ground simulation of hypervelocity space debris impacts on polymers; R. Verker et al. Testing of spacecraft materials for long duration flights in low earth orbit; L.S. Novikov et al. M/OD impacts on the multi-purpose logistics module: post flight inspection results; J.L. Hyde, R.P. Bernhard, E.L. Christiansen. Fuel oxidizer reaction products (FORP) contamination of service module and release of N-nitrosodimethylamine in a humid environment from crew EVA suits contaminated with FORP; W. Schmidl et al. Effect of vacuum thermocycling on properties of unidirectional M40J/AG-80 Composites; Y. Gao et al. Damage characteristics of Zr 41 Ti 14 Cu 12.5 Ni 10 Be 22.5 bulk metallic glass impacted by hypervelocity projectiles; C. Yang et al . Effect of VUV radiation on properties and chemical structure of polyethylene terephthalate film; G. Peng, D. Yang, S. Y. He. Section C. Status of solar sail material characterization at NASA s Marshall Space Flight Center; D. Edwards et al. Atomic oxygen durability evaluation of a UV curable ceramer protective coating ; B.A. Banks et al . Cermet thermal conversion coatings for space applications; B. W. Woods et al. Multi-function smart coatings for space applications; R.V. Kruzelecky et al. Effects of space environment exposure on the blocking force of silicone adhesive; P. Boeder et al. Dry sliding wear of Ti-6Al-4V Alloy at low temperature in vacuum; Y. Liu et al. Section D. Erosion of Kapton H by hyperthermal atomic oxygen: Dependence on O-atom fluence and surface temperature; D.M. Buczala, T. K. Minton. Transparent arcproof protective coatings - performance and manufacturability issues; J. Griffin et al. The dtudy of the rffects of stomic oxygen erosion on the microstructure and property of VO 2 thermochromic coating using CSA s space simulation apparatus; X.X. Jiang et al. Section E. Damage kinetics of quartz glass by proton radiation; Q. Wei, S.Y. He, D. Yang. Microscopic mechanisms and dynamics simulations of O + ( 4 S 3/2 ) reacting with methane; L. Sun, G. Schatz. Theoretical study of reactions of hyperthermal O( 3 P) with perfluorinated hydrocarbons; D. Troya, G.C. Schatz. Simulation of UV influence on outgassing of polymer composites; R.H. Khassanchine et al. The impact of high-velocity particles on thermal pipelines in spacecraft; N.D. Semkin, K.E. Voronov, L.S. Novi
Introduction. Acknowledgements. Organization. Section A. Radiation effects of protons and electrons on Back-field silicon solar cells; Z. Hu, S. He, D. Yang . Solar array arcing in LEO: how much charge is discharged?; D.C. Ferguson, B.V. Vayner, J.T. Galofaro. Self-restoration as SEU protection mechanism for re-configurable on-board computing platform; L. Kirischian, et al . Synergistic effects of protons and electrons on radiation damage of methyl silicone rubber; L. Zhang et al . Influence of electron radiation on outgassing of spacecraft materials; R. H. Khassanchineet al . Effect of surface charging on the erosion rate of polyimide under 5 eV atomic oxygen beam exposure; M. Tagawa et al . Influence of space environment on spectral optical properties of thermal control coatings; V.M. Prosvirikov, et al. Mitigation of thruster plume-induced erosion of ISS sensitive hardware; C. Pankop, J. Alred, P. Boeder . Degradation of thermal control coatings under influence of proton irradiation; L.S. Noviko et al . Mitigation of damage to the international space station (ISS) from water dumps; W. Schmidl, J. Visentine, R. Mikatarian . Investigation of synergistic effects of proton and electron radiation on the dyeing of optical quartz glass; H. Liu et al . The role of "abnormal" electron fluxes with energy < 1 MeV in the surface charging dose of spacecraft; O.R. Grigoryan et al. Section B. Vacuum ultraviolet radiation effects on DC93-500 silicone film; J.A. Dever, B.A. Banks, L. Yan .Enhancement of atomic oxygen-induced erosion of spacecraft polymeric materials by simultaneous ultraviolet exposure; K. Yokota, N. Ohmae, M. Tagawa. ground simulation of hypervelocity space debris impacts on polymers; R. Verker et al. Testing of spacecraft materials for long duration flights in low earth orbit; L.S. Novikov et al. M/OD impacts on the multi-purpose logistics module: post flight inspection results; J.L. Hyde, R.P. Bernhard, E.L. Christiansen. Fuel oxidizer reaction products (FORP) contamination of service module and release of N-nitrosodimethylamine in a humid environment from crew EVA suits contaminated with FORP; W. Schmidl et al. Effect of vacuum thermocycling on properties of unidirectional M40J/AG-80 Composites; Y. Gao et al. Damage characteristics of Zr 41 Ti 14 Cu 12.5 Ni 10 Be 22.5 bulk metallic glass impacted by hypervelocity projectiles; C. Yang et al . Effect of VUV radiation on properties and chemical structure of polyethylene terephthalate film; G. Peng, D. Yang, S. Y. He. Section C. Status of solar sail material characterization at NASA s Marshall Space Flight Center; D. Edwards et al. Atomic oxygen durability evaluation of a UV curable ceramer protective coating ; B.A. Banks et al . Cermet thermal conversion coatings for space applications; B. W. Woods et al. Multi-function smart coatings for space applications; R.V. Kruzelecky et al. Effects of space environment exposure on the blocking force of silicone adhesive; P. Boeder et al. Dry sliding wear of Ti-6Al-4V Alloy at low temperature in vacuum; Y. Liu et al. Section D. Erosion of Kapton H by hyperthermal atomic oxygen: Dependence on O-atom fluence and surface temperature; D.M. Buczala, T. K. Minton. Transparent arcproof protective coatings - performance and manufacturability issues; J. Griffin et al. The dtudy of the rffects of stomic oxygen erosion on the microstructure and property of VO 2 thermochromic coating using CSA s space simulation apparatus; X.X. Jiang et al. Section E. Damage kinetics of quartz glass by proton radiation; Q. Wei, S.Y. He, D. Yang. Microscopic mechanisms and dynamics simulations of O + ( 4 S 3/2 ) reacting with methane; L. Sun, G. Schatz. Theoretical study of reactions of hyperthermal O( 3 P) with perfluorinated hydrocarbons; D. Troya, G.C. Schatz. Simulation of UV influence on outgassing of polymer composites; R.H. Khassanchine et al. The impact of high-velocity particles on thermal pipelines in spacecraft; N.D. Semkin, K.E. Voronov, L.S. Novi
Rezensionen
"However, any of our readers who develop materials or devices for spacecraft applications, or universities that study materials for space applications, May find some of the papers in this bookto be useful for the development of new materials and/or give guidance in material testing for the space environment as well as in regard to knowing the degradation rates of various materials in the space environment." -- Electrical Insulation Magazine, July/August 2007 - Vol.23, No.4 p.65
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