Protection of Materials and Structures from the Low Earth Orbit Space Environment: Proceedings of ICPMSE-3, Third International Space Conference, held in Toronto, Canada, April 25–26, 1996: Space Technology Proceedings, cartea 2
Editat de J. Kleiman, R.C. Tennysonen Limba Engleză Paperback – 11 oct 2012
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Specificații
ISBN-13: 9789401060042
ISBN-10: 9401060045
Pagini: 276
Ilustrații: X, 262 p.
Dimensiuni: 160 x 240 x 14 mm
Greutate: 0.4 kg
Ediția:Softcover reprint of the original 1st ed. 1999
Editura: SPRINGER NETHERLANDS
Colecția Springer
Seria Space Technology Proceedings
Locul publicării:Dordrecht, Netherlands
ISBN-10: 9401060045
Pagini: 276
Ilustrații: X, 262 p.
Dimensiuni: 160 x 240 x 14 mm
Greutate: 0.4 kg
Ediția:Softcover reprint of the original 1st ed. 1999
Editura: SPRINGER NETHERLANDS
Colecția Springer
Seria Space Technology Proceedings
Locul publicării:Dordrecht, Netherlands
Public țintă
ResearchCuprins
Section A AO/VUV and Radiation Effects on Materials and Structures in the Leo Space Environment.- 10.1007/978-94-011-4768-2_1[1] Low Flux Atomic Oxygen: Can it be More Hazardous than High Flux? A Risk Assessment Study.- 10.1007/978-94-011-4768-2_2[2] Atomic Oxygen Durability Testing of an International Space Station Solar Array Validation Coupon.- 10.1007/978-94-011-4768-2_3[3] A Technique for Synergistic Atomic Oxygen and Vacuum Ultraviolet Radiation Durability.- 10.1007/978-94-011-4768-2_4[4] Atomic Oxygen Durability of Second Surface Silver Microsheet Glass Concentrators.- 10.1007/978-94-011-4768-2_5[5] A Study of Atomic Oxygen Material Degradation by Spaceflight Experiments and Ground-Based Simulation.- 10.1007/978-94-011-4768-2_6[6] Laboratory Simulation of Low Earth Orbit.- Section B: Interaction of Matter with LEO Environment.- 10.1007/978-94-011-4768-2_7[7] Prediction of In-Space Durability of Protected Polymers Based on Ground Laboratory Thermal Energy Atomic Oxygen Testing.- 10.1007/978-94-011-4768-2_8[8] Ground-Based Experimental Verification of the Predictive Model of Polymer-Based Materials Erosion by Atomic Oxygen in LEO.- 10.1007/978-94-011-4768-2_9[9] Anomalous Behaviour of the Linear Expansion Coefficient of Reinforced Plastics at Increased Temperatures.- 10.1007/978-94-011-4768-2_10[10] Predictive Models of Erosion Processes in LEO Space Environment: A Basis for Development of an Engineering Software.- Section C Large Scale Coating Process Developments for Protection in LEO.- 10.1007/978-94-011-4768-2_11[11] The Strategic Technologies for Automation and Robotics (Stear) Program: Protection Of Materials In The Space Environment Sub-Program.- 10.1007/978-94-011-4768-2_12[12] Plasma-Deposited Coatings for the Protection of Spacecraft Material Against Atomic Oxygen Erosion.- 10.1007/978-94-011-4768-2_13[13] Large-Scale Electron Cyclotron Resonance Deposition of Protective Coatings for Space Applications.- 10.1007/978-94-011-4768-2_14[14] Development of High Diffuse Reflectance Surfaces on Teflon.- 10.1007/978-94-011-4768-2_15[15] Materials Exposure in Low Earth Orbit 2 (MELEO2): An Update.- 10.1007/978-94-011-4768-2_16[16] Protection of the Radarsat Spacecraft from the Low Earth Oribt Environment.- Section D Synthesis and Modification of Materials and Surfaces for Protection in LEO.- 10.1007/978-94-011-4768-2_17[17] About Some Aspects of Changing Optical Properties of Glass in Solar Arrays and other Space Materials on Exposure to Leo Space Environment.- 10.1007/978-94-011-4768-2_18[18] Photosil™ - A New Surface Modification Technique for Erosion Resistance Improvement of Polymer-Based Materials in Leo.- 10.1007/978-94-011-4768-2_19[19] Soft X-Ray Radiation as a Factor in the Degradation of Spacecraft Materials.- 10.1007/978-94-011-4768-2_20[20] Surface Modification of Polymer-Based Materials by Ion Implantation: A New Approach for Protection in LEO.- 10.1007/978-94-011-4768-2_21[21] TOR and COR AO-VUV Resistant Polymers for Space.