Protection of Materials and Structures from the Space Environment
Springer (Verlag)
978-94-007-8854-1 (ISBN)
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 | 28.11.2014 |
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Reihe/Serie | Space Technology Proceedings ; 6 |
Zusatzinfo | XIV, 462 p. |
Verlagsort | Dordrecht |
Sprache | englisch |
Maße | 155 x 235 mm |
Themenwelt | Naturwissenschaften ► Chemie ► Organische Chemie |
Technik ► Fahrzeugbau / Schiffbau | |
Technik ► Luft- / Raumfahrttechnik | |
Technik ► Maschinenbau | |
ISBN-10 | 94-007-8854-1 / 9400788541 |
ISBN-13 | 978-94-007-8854-1 / 9789400788541 |
Zustand | Neuware |
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