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
Published on 28. February 1999
Book
Hardback
X, 262 pages
978-0-7923-5540-3 (ISBN)
Description
This publication presents the proceedings of ICPMSE-3, the third international conference on Protection of Materials and Structures from the Low Earth Orbit Space Environment, held in Toronto April 25-26, 1996. The conference was hosted and organized by Integrity Testing Laboratory Inc, (ITL), and held at the University of Toronto's Institute for Aerospace Studies (UTIAS), where ITL is located. Twenty industrial companies, seven wliversities and eight government agencies from Canada, USA, United Kingdom, France, Israel, Russia, Ukraine and the Netherlands were represented by over 55 participants indicating increasing international co-operation in this critical arena of protection of materials in space. Twenty-five speakers, world experts in their fields, delivered talks on a wide variety of topics on various aspects of material protection in space, Representatives from the Canadian, American, European and Israeli space agencies as well as from leading space research laboratories of major aerospace industries gathered at UTIAS to discuss the latest developments in the field of material and structure protection from the harsh space environment, These proceedings are organized into four sections: a) AONOV and Radiation Effects on Materials and Structures in the Leo Space Environment; b) Interaction of Matter with the LEO Environment; c) Large Scale Coating Process Developments for Protection in LEO; d) Synthesis and Modification of Materials and Surfaces for Protection in LEO, This is the third in our on-going series of bi-annual international space materials conferences wllich began in 1992 in Toronto. Jacob Kleiman, Integrity Testing Laboratory Inc.
More details
Series
Edition
1999 ed.
Language
English
Place of publication
Dordrecht
Netherlands
Target group
College/higher education
Professional and scholarly
Illustrations
X, 262 p.
Dimensions
Height: 241 mm
Width: 160 mm
Thickness: 20 mm
Weight
582 gr
ISBN-13
978-0-7923-5540-3 (9780792355403)
DOI
10.1007/978-94-011-4768-2
Schweitzer Classification
Other editions
Additional editions
J. Kleiman | R.C. Tennyson
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
E-Book
11/2013
Springer
€213.99
Available for download
J. Kleiman | R.C. Tennyson
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
Book
10/2012
Springer
€213.99
Shipment within 15-20 days
Content
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] PhotosilT - 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.