Protection of Materials and Structures from the Space Environment
Springer-Verlag New York Inc.
978-1-4020-4281-2 (ISBN)
ThispublicationpresentstheproceedingsofICPMSE-7,theSeventhInternational Conference on Protection of Materials and Structures from Space Environment, held in Toronto May 10–13, 2004. The ICPMSE series of meetings became an important part of the LEO space communitysinceitwasstartedin1991.Sincethen,themeetinghasgrownsteadily, establishing itself as the only North American event covering the various aspects of materials protection in LEO and attracting a large number of engineers, - searchers, managers, and scientists from industrial companies, scienti?c insti- tionsandgovernmentagenciesinCanada,USA,Asia,andEurope,thusbecoming a true international event. The ICPMSE-7 meeting continued the tradition of the previous meetings including in the program the topics on protection of materials in GEO and Deep Space. The conference was organized by Integrity Testing Laboratory Inc. (ITL), and hosted by the University of Toronto’s Institute for Aerospace Studies (UTIAS). The meeting was sponsored by: a) The Materials and Manufacturing Ontario (MMO) and the CRESTech, two Ontario Centres of Excellence that from April 1, 2004 joined under the - tario Centres of Excellence Inc. (OCE Inc) a not-for-pro?t, member-based corporation dedicated to establishing Ontario as the place to be for innovation; b) MD Robotics; c) The Integrity Testing Laboratory (ITL) and d) The University of Toronto Institute for Aerospace Studies (UTIAS). Over 80 people from countries covering the American, European and Asian continents registered for the conference representing the major space agencies and the major companies, institutions and government organizations involved in space activities, indicating a further increase in international co-operation in this critical area of protection of materials inspace.
RADIATION EFFECTS OF PROTONS AND ELECTRONS ON BACKFIELD SILICON SOLAR CELLS.- SOLAR ARRAY ARCING IN LEO: How Much Charge is Discharged?.- SELF-RESTORATION AS SEU PROTECTION MECHANISM FOR RECONFIGURABLE ON-BOARD COMPUTING PLATFORM.- SYNERGISTIC EFFECT OF PROTONS AND ELECTRONS ON RADIATION DAMAGE OF METHYL SILICONE RUBBER.- INFLUENCE OF ELECTRON RADIATION ON OUTGASSING OF SPACECRAFT MATERIALS.- EFFECT OF SURFACE CHARGING ON THE EROSION RATE OF POLYIMIDE UNDER 5 EV ATOMIC OXYGEN BEAM EXPOSURE.- INFLUENCE OF SPACE ENVIRONMENT ON SPECTRAL OPTICAL PROPERTIES OF THERMAL CONTROL COATINGS.- MITIGATION OF THRUSTER PLUME-INDUCED EROSION OF ISS SENSITIVE HARDWARE.- DEGRADATION OF THERMAL CONTROL COATINGS UNDER INFLUENCE OF PROTON IRRADIATION.- MITIGATION OF DAMAGE TO THE INTERNATIONAL SPACE STATION (ISS) FROM WATER DUMPS.- INVESTIGATION OF SYNERGISTIC EFFECTS OF PROTON AND ELECTRON RADIATION ON THE DYEING OF OPTICAL QUARTZ GLASS.- THE ROLE OF “ABNORMAL” ELECTRON FLUXES WITH ENERGY <1 MeV IN THE SURFACE CHARGING DOSE OF SPACECRAFT.- VACUUM ULTRAVIOLET RADIATION EFFECTS ON DC93-500 SILICONE FILM.- ENHANCEMENT OF ATOMIC OXYGEN-INDUCED EROSION OF SPACECRAFT POLYMERIC MATERIALS BY SIMULTANEOUS ULTRAVIOLET EXPOSURE.- GROUND SIMULATION OF HYPERVELOCITY SPACE DEBRIS IMPACTS ON POLYMERS.- TESTING OF SPACECRAFT MATERIALS FOR LONG FLIGHTS IN LOW EARTH ORBIT.- M/OD IMPACTS ON THE MULTIPURPOSE LOGISTICS MODULE: Post Flight Inspection Results.- 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.- EFFECT OF VACUUM THERMOCYCLING ON PROPERTIES OF UNIDIRECTIONAL M40J/AG-80 COMPOSITES.- DAMAGE CHARACTERISTICS OF Zr41Ti14Cu12.5Ni10Be22.5 BULK METALLIC GLASS IMPACTED BYHYPERVELOCITY PROJECTILES.- EFFECT OF VUV RADIATION ON PROPERTIES AND CHEMICAL STRUCTURE OF POLYETHYLENE TEREPHTHALATE FILM.- STATUS OF SOLAR SAIL MATERIAL CHARACTERIZATION AT NASA’S MARSHALL SPACE FLIGHT CENTER.- ATOMIC OXYGEN DURABILITY EVALUATION OF A UV CURABLE CERAMER PROTECTIVE COATING.- CERMET THERMAL CONVERSION COATINGS FOR SPACE APPLICATIONS.- MULTIFUNCTION SMART COATINGS FOR SPACE APPLICATIONS.- EFFECTS OF SPACE ENVIRONMENT EXPOSURE ON THE BLOCKING FORCE OF SILICONE ADHESIVE.- DRY SLIDING WEAR OF Ti-6Al-4V ALLOY AT LOWTEMPERATURE IN VACUUM.- EROSION OF KAPTON H BY HYPERTHERMAL ATOMIC OXYGEN: DEPENDENCE ON O-ATOM FLUENCE AND SURFACE TEMPERATURE.- TRANSPARENT ARCPROOF PROTECTIVE COATINGS: PERFORMANCE AND MANUFACTURABILITY ISSUES.- THE STUDY OF THE EFFECTS OF ATOMIC OXYGEN EROSION ON THE MICROSTRUCTURE AND PROPERTY OF VO2 THERMOCHROMIC COATING USING CSA’S SPACE SIMULATION APPARATUS.- DAMAGE KINETICS OF QUARTZ GLASS BY PROTON RADIATION.- MICROSCOPIC MECHANISMS AND DYNAMICS SIMULATIONS OF O+(4S3/2) REACTING WITH METHANE.- THEORETICAL STUDY OF REACTIONS OF HYPERTHERMAL O(3P)WITH PERFLUORINATED HYDROCARBONS.- SIMULATION OF UV INFLUENCE ON OUTGASSING OF POLYMER COMPOSITES.- THE IMPACT OF HIGH-VELOCITY PARTICLES ON THERMAL PIPELINES IN SPACECRAFT.- PHYSICAL MECHANISM OF SOLAR CELL SHUNTING UNDER HIGH VELOCITY IMPACT OF SOLID PARTICLES.- DETERMINATION OF GROUND-LABORATORY TO IN-SPACE EFFECTIVE ATOMIC OXYGEN FLUENCE FOR DC 93-500 SILICONE.- ATOMIC OXYGEN CONCENTRATION USING REFLECTING MIRRORS.- ATOMIC OXYGEN SOURCE CALIBRATION ISSUES: A UNIVERSAL APPROACH.- LOW-COST SPACE MISSIONS FOR SCIENTIFIC AND TECHNOLOGICAL INVESTIGATIONS.
| Erscheint lt. Verlag | 20.9.2006 |
|---|---|
| Reihe/Serie | Space Technology Proceedings ; 6 |
| Zusatzinfo | XIV, 462 p. |
| Verlagsort | New York, NY |
| Sprache | englisch |
| Maße | 160 x 240 mm |
| Themenwelt | Technik ► Fahrzeugbau / Schiffbau |
| Technik ► Luft- / Raumfahrttechnik | |
| Technik ► Maschinenbau | |
| ISBN-10 | 1-4020-4281-7 / 1402042817 |
| ISBN-13 | 978-1-4020-4281-2 / 9781402042812 |
| Zustand | Neuware |
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