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Protection of Space Materials from the Space Environment J. Kleiman

Protection of Space Materials from the Space Environment By J. Kleiman

Protection of Space Materials from the Space Environment by J. Kleiman


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Summary

Proceedings of ICPMSE-4, Fourth International Space Conference, held in Toronto, Canada, April 23-24, 1998

Protection of Space Materials from the Space Environment Summary

Protection of Space Materials from the Space Environment: Proceedings of ICPMSE-4, Fourth International Space Conference, held in Toronto, Canada, April 23-24, 1998 by J. Kleiman

This publication presents the proceedings of ICPMSE-4, the fourth international conference on Protection of Materials and Structures from the Low Earth Orbit Space Environment, held in Toronto April 23-24, 1998. The conference was hosted and organized by Integrity Testing Laboratory Inc. (ITL), and held at the University ofToronto's Institute for Aerospace Studies (UTIAS). Twenty two industrial companies, six universities and fourteen government agencies from Canada, USA, United Kingdom, France, Israel, Russia, Ukraine and the Netherlands were represented by over 75 participants indicating increasing international co-operation in this critical arena of protection of materials in space. Twenty-seven speakers, world experts in their fields, delivered talks on a wide variety of topics on various aspects of material protection in space. Representatives from the Canadian, American, European and Israeli space agencies as well as from leading space research laboratories ofmajor aerospace industries gathered at UTIAS to discuss the latest developments in the field of material and structure protection from the harsh space environment.

Table of Contents

Acknowledgements. Introduction. Organizing Committee. Section A: AO/VUV Effects, Evaluation and Modeling. 1. Monte Carlo Computational Modeling of the Energy Dependence of Atomic Oxygen Undercutting of Protected Polymers; B.A. Banks, et al. 2. Dynamics of Atomic-Oxygen-Induced Degradation of Materials; T.K. Minton, et al. 3. Generalization of the Predictive Model of Erosion of Carbon-Based Materials by Atomic Oxygen; J.I. Kleiman, et al. 4. Spectroscopic Ellipsometry Characterization of Polymers Modified by Atomic Oxygen and Ultraviolet Radiation; C.L. Bungay, et al. 5. Effect of Atomic Oxygen Exposures on the Tribological Properties of Molybdenum Disulfide Lubricants; M. Tagawa, et al. 6. Influence of Shielding Upon the Structure and Properties of Polymer Composite Materials, Exposed on the Surface of the Mir Orbital Complex; O.V. Startsev, et al. 7. Cleanliness Support of Vehicle Fairings for Spacecraft; V. Sitalo, V. Tikhiy. 8. In situ XPS Studies of Kapton Exposed to 5 eV Atomic Oxygen; E. Grossman, et al. Section B: Instrumentation, Sensors, New Technologies. 9. A Low Cost, Lightweight Reusable Sensor for Atomic Oxygen Detection; J.J. Osborne, et al. 10. Large-Scale ECR-CVD Preparation of Integrated Thin-Film Structures for Space Applications; R.V. Kruzelecky, et al. 11. Non-Silicone Inorganic Polymer-Based Coatings for Atomic Oxygen Protection in LEO - Part 2; E. Poire, et al. 12. Research Aspects of Scaling Up the Implantox Technology for Protection of Polymers in Space; Z.A. Iskanderova, et al. Section C: ThermalControl in LEO. 13. A Comparison of Space and Ground-Based Facility Environmental Effects for FEP Teflon; S.K. Rutledge, et al. 14. Evaluation of Low Earth Orbit Environmental Effects on International Space Station Thermal Control Materials; J.A. Dever, et al. 15. Some Aspects of the Degradation of FEP Teflon Material Under the Action of VUV, the Sun and Ground Test VUV Facilities; A. Milintchouk, M. Van Eesbeek. 16. Evaluation of COF MDPS Chromic Acid Anodization in LEO Environment; C. Acket, et al. 17. A Database for the Selection of Surfaces and Materials for Space and Ground-based Applications; S.H. McCall, et al. 18. Thermal Control Materials and Coatings Currently Being Developed in France for Use in Low Earth Orbit; F. Guerard, J.C. Guillaumon. 19. Modification of Thermal Control Paints by Photosil (TM) Technology; J.I. Kleiman, et al. Section D: Charged Particles/Soft X-Rays/Meteoroids/Thermal Cycling. 20. Simulated Solar Flare X-Ray and Thermal Cycling Durability Evaluation of HST Thermal Control Candidate Replacement Materials; K.K. de Groh, et al. 21. Radiation-Induced Effects in SiO2 Protective Coatings on Polymeric Spacecraft Materials; C. Coia, et al. 22. Influence of Electron and Proton Fluxes on Optical Properties of Protective Enamel; S.N. Skovorod'ko, et al. 23. Meteoroid Hazard in the LEO Space Environment; Y.S. Yatskiv, et al. 24. Characterizing the Annual Meteoroid Streams; M. Beech. 25. Oxidation Kinetics of VB Group Metals by Atomic and Molecular Oxygen; A.G. Gusakov, et al. 26.

Additional information

NPB9780792369813
9780792369813
0792369815
Protection of Space Materials from the Space Environment: Proceedings of ICPMSE-4, Fourth International Space Conference, held in Toronto, Canada, April 23-24, 1998 by J. Kleiman
New
Hardback
Springer
2001-06-30
359
N/A
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