Protection of Materials and Structures from Space Environment

ICPMSE-6

Editors:

ISBN: 978-1-4020-1690-5 (Print) 978-1-4020-2595-2 (Online)

Table of contents (50 chapters)

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  1. Section A

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      Pages 1-5

      A New Era for Canada in Space

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      Pages 7-29

      Space and Atmospheric Environments: From Low Earth Orbits to Deep Space

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      Pages 31-72

      Materials Interactions with Space Environment: International Space Station - May 2000 to May 2002

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      Pages 73-80

      Photoconductivity in Transparent Arcproof Coatings

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      Pages 81-89

      Effects of Space Environment Factors on Optical Materials for Space Application

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      Pages 91-98

      A Study of Synergistic Radiation Effects of Protons and Electrons on Teflon FEP/Al Degradation

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      Pages 99-111

      Dose Rate Effects in Polymer Materials Irradiated in Vacuum

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      Pages 113-122

      Towards a Database for Assessment of Near-Earth Space Radiation Effects on Optical Glasses

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      Pages 123-131

      The Role of Proton and Electron “Abnormal” Formations in Radiation Impact on Construction Elements of Spacecrafts

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      Pages 131-137

      A Study of Methylsilicone Rubber Damage Behavior Induced by Proton Irradiation

  2. Section B

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      Pages 139-154

      A Unified Space Environment Effects Database for Russian and North American Organic and Inorganic Materials

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      Pages 155-169

      The Effect of Heating on the Degradation of Ground Laboratory and Space Irradiated Teflon FEP

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      Pages 171-181

      On the Thermal Stability of Polyimides for Space Application

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      Pages 183-191

      Synergistic Degradation of CV-1144-O Due to Ultraviolet Radiation and Heat

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      Pages 193-201

      Behaviour of Thermal Control Coatings Under Atomic Oxygen and Ultraviolet Radiation

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      Pages 203-216

      Ground Testing of SCK5 White Silicone Paint for LEO Applications

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      Pages 217-233

      Study of Polymer Coatings Resistance After the Longterm Exposure on Space Station “MIR”

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      Pages 235-243

      Issues and Consequences of Atomic Oxygen Undercutting of Protected Polymers in Low Eerth Orbit

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      Pages 245-255

      Effect of Space Gaseous Environment on the Thermophysical Properties of Materials and Structures

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      Pages 257-262

      CLeanliness Support of the Launch Vehicle for Putting into Orbit the Spacecraft Meteor-3M with the “Sage-III” Instrument

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