Protection of Materials and Structures from Space Environment ICPMSE-6 /
This publication presents the proceedings of ICPMSE-6, the sixth international conference on Protection of Materials and Structures from Space Environment, held in Toronto May 1-3, 2002. The ICPMSE series of meetings became an important part of the LEO space community since it was started in 1991. S...
| Συγγραφή απο Οργανισμό/Αρχή: | |
|---|---|
| Άλλοι συγγραφείς: | , |
| Μορφή: | Ηλεκτρονική πηγή Ηλ. βιβλίο |
| Γλώσσα: | English |
| Έκδοση: |
Dordrecht :
Springer Netherlands,
2003.
|
| Σειρά: | Space Technology Proceedings,
5 |
| Θέματα: | |
| Διαθέσιμο Online: | Full Text via HEAL-Link |
Πίνακας περιεχομένων:
- Section A
- A New Era for Canada in Space
- Space and Atmospheric Environments: From Low Earth Orbits to Deep Space
- Materials Interactions with Space Environment: International Space Station - May 2000 to May 2002
- Photoconductivity in Transparent Arcproof Coatings
- Effects of Space Environment Factors on Optical Materials for Space Application
- A Study of Synergistic Radiation Effects of Protons and Electrons on Teflon FEP/Al Degradation
- Dose Rate Effects in Polymer Materials Irradiated in Vacuum
- Towards a Database for Assessment of Near-Earth Space Radiation Effects on Optical Glasses
- The Role of Proton and Electron “Abnormal” Formations in Radiation Impact on Construction Elements of Spacecrafts
- A Study of Methylsilicone Rubber Damage Behavior Induced by Proton Irradiation
- Section B
- A Unified Space Environment Effects Database for Russian and North American Organic and Inorganic Materials
- The Effect of Heating on the Degradation of Ground Laboratory and Space Irradiated Teflon FEP
- On the Thermal Stability of Polyimides for Space Application
- Synergistic Degradation of CV-1144-O Due to Ultraviolet Radiation and Heat
- Behaviour of Thermal Control Coatings Under Atomic Oxygen and Ultraviolet Radiation
- Ground Testing of SCK5 White Silicone Paint for LEO Applications
- Study of Polymer Coatings Resistance After the Longterm Exposure on Space Station “MIR”
- Issues and Consequences of Atomic Oxygen Undercutting of Protected Polymers in Low Eerth Orbit
- Effect of Space Gaseous Environment on the Thermophysical Properties of Materials and Structures
- CLeanliness Support of the Launch Vehicle for Putting into Orbit the Spacecraft Meteor-3M with the “Sage-III” Instrument
- Section C
- Irreversible Shrinkage Effects of Carbon Fibers in Polymer Matrix Composites Exposed to the “MIR” Space Enuironment
- Combined Effect of Thermal and Mechanical Stresses on the Viscoelastic Properties of a Composite Material for Space Structures
- Hyperthermal Reactions of Oxygen Atoms with Saturated Hydrocarbons
- A Review of Lubrication on the Canadarm 2
- Degradation of Polymers by O(3P) in Low Earth Orbit
- Iridium Metal as Potential Substrates for Experiments in Space
- The Influence of the Atomic Oxygen Plasma on the Surface and on the Photoelectric Properties of Solar Arrays
- Some Aspects of Simulation of Outgassing Processes in Thermal Vacuum Exposure of Coatings Applied to Space
- Section D
- Vacuum Ultraviolet Radiation Characterization of RF Air Plasma and Effects on Polymer Films
- Studies of the Surface Oxidation of Silver by Atomic Oxygen
- Determination of the Energy Level of the Atomic Oxygen Flux Generated by the Space Simulation Apparatus Using a Thermal Modeling Method
- Design and Testing of a Mini-spectrometer System for On-Orbit Degradation Studies of Optical Materials
- Kapton as a Standard for Atomic Oxygen Flux Measurement in LEO Ground Simulation Facilities: How Good Is It?
- Temperature and Impingement Angle Dependences of Atomic Oxygen-Induced Erosion of Polyimide and Polyethylene Films Measured by Quartz Crystal Microbalance
- Integrating Sphere Unit for Precision Measurement of Absolute Reflectance and Transmittance of Spacecraft Materials in a Vacuum Chamber
- Numerical Simulation of Thermal Stress Induced by Thermocycling in Hot Rolled 1420 Al-Li Alloy
- Changes in Microstructure and Tensile Properties of Hot Rolled 1420 Al-Li Alloy Subjected to Thermocycling
- Section E
- Photosil™ Surface Modification Treatment of Polymer-based Space Materials and External Space Components
- Atomic Oxygen Resistant, Low Alpha, Anti-static Polyimides for Potential Space Applications
- Deposition and Characteristics of Atomic Oxygen Protective Coatings Using Plasma Polymerized HMDSO
- Development of Protective and Passive Thermal Control Coatings on Carbon-based Composite Materials for Application in Space
- Structure and Composition of Non-Metallic Solar Array Materials Retrieved After Long-Term Exposure Overboard the “MIR” Orbital Space Station
- Micro- and Macrotribological Properties of Solid Lubricants in 5 Electronvolts Atomic Oxygen Exposures
- ZnSe Coatings for Spacecraft Electrochromic Thermal Control Surfaces
- Perfluorocyclobutane (PFCB) Polyaryl Ethers for Space-based Applications
- Section F
- Fast Three-Dimensional Method of Modeling Atomic Oxygen Undercutting of Protected Polymers
- Development and Verification of a Predictive Model and Engineering Software Guide for Durability Evaluation of Polymer-Based Materials in LEO
- Comparative Study of Low Energy C and O Atoms Impact in a Hydrocarbon Surface
- A Direct Trajectory Dynamics Investigation of Fast O+ Alkane Reactions
- Mathematical Simulation Methods to Predict Changes of Integral and Spectral Optical Surface Characteristics of External Spacecraft Materials and Coatings.
