Protection of Materials and Structures from the Space Environment (eBook, PDF)

ICPMSE-7
Redaktion: Kleiman, Jacob I.

• Format: PDF

Produktbeschreibung

The goals of the ICPMSE-7 meeting, as in the past years, are to facilitate exchanges between members of the various engineering disciplines involved in development of space materials, including such aspects as environmental hazards of Low Earth Orbit (LEO), Geostationary Earth Orbit (GEO) and Deep Space, ground-based qualification, and in-flight experiments and lessons learned from operational vehicles.

The book continues to discuss topics started in the earlier publications and adds new data and results.

The proceedings cover a range of inter-disciplinary topics concerning the protection of materials and structures in space and discussing the effects of the aggressive LEO as well as the GEO and Deep Space environments on materials and structures and the ways to predict and reduce these effects in short and long-term space missions.

The book is targeting organizations and individuals involved with space material selction, their reliability and influence of space environmental effects on materials and structures.

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Dieser Download kann aus rechtlichen Gründen nur mit Rechnungsadresse in A, B, BG, CY, CZ, D, DK, EW, E, FIN, F, GR, HR, H, IRL, I, LT, L, LR, M, NL, PL, P, R, S, SLO, SK ausgeliefert werden.

Produktdetails

• Verlag: Springer Netherlands
• Seitenzahl: 462
• Erscheinungstermin: 13. Juli 2006
• Englisch
• ISBN-13: 9781402043192
• Artikelnr.: 37352765

Inhaltsangabe

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.

Rezensionen

"However, any of our readers who develop materials or devices for spacecraft applications, or universities that study materials for space applications, May find some of the papers in this bookto be useful for the development of new materials and/or give guidance in material testing for the space environment as well as in regard to knowing the degradation rates of various materials in the space environment."
Electrical Insulation Magazine, July/August 2007 - Vol.23, No.4 p.65