Protection of Materials and Structures from the Space Environment: ICPMSE-7Jacob I. Kleiman Springer Science & Business Media, 13. júl. 2006 - 462 síður 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 in space. |
Efni
9 | |
SelfRestoration as SEU Protection Mechanism for Reconfigurable | 20 |
Kirischian V Geurkov I Terterian and J Kleiman | 34 |
Zhang S He D Yang and Q | 43 |
Effect of Surface Charging on the Erosion Rate of Polyimide | 51 |
Tagawa S Seikyu K I Maeda K Yokota and N Ohmae | 60 |
A P Zelenkevich and V M Tsvelev | 71 |
Degradation of Thermal Control Coatings Under Influence | 86 |
Atomic Oxygen Durability Evaluation of a UV Curable Ceramer | 247 |
B A Banks C A Karniotis D Dworak and M Soucek | 264 |
Kruzelecky E Haddad B Wong W Jamroz M Soltani | 295 |
Dry Sliding Wear of Ti6Al4V Alloy at Low Temperature | 308 |
Performance | 331 |
Kruzelecky and E Haddad | 351 |
Sun and G C Schatz | 365 |
The Impact of HighVelocity Particles on Thermal Pipelines | 384 |
W Schmidl J Visentine and R Mikatarian | 106 |
Vacuum Ultraviolet Radiation Effects on DC93500 Silicone Film | 123 |
Enhancement of Atomic OxygenInduced Erosion of Spacecraft | 141 |
Pankop J Alred and P Boeder | 166 |
Hyde R P Bernhard and E L Christinsen | 193 |
Effect of Vacuum Thermocycling on Properties of Unidirectional | 209 |
Yang C Z Fan Y Z Jia X Y Wang | 225 |
A Letin A B Nadiradze and L S Novikov | 400 |
K K De Groh B A Banks and D | 417 |
Tagawa K Matsumoto H Doi K Yokota and N Ohmae | 431 |
Rankin R E Zee F M Pranajaya D G Foisy | 442 |
Author Index | 461 |
Aðrar útgáfur - View all
Protection of Materials and Structures from the Space Environment: ICPMSE-7 Jacob I. Kleiman Engin sýnishorn í boði - 2014 |
Protection of Materials and Structures from the Space Environment: ICPMSE-7 Jacob I. Kleiman Engin sýnishorn í boði - 2006 |
Common terms and phrases
absorption adhesive aluminum atomic oxygen atomic oxygen exposure atomic oxygen flux blackbody calculated cermet coating color centers composition concentration contact depth damage degradation deposition diameter dose effective fluence emissivity energy erosion erosion rate experimental exposed flight fluence FORP FPGA fracture hyperthermal hypervelocity incident angle increase intensity irradiation J.I. Kleiman Kapton Kapton effective Kapton H laser layer low Earth orbit mass loss Materials and Structures measured mechanical Meteoroid MPLM NASA NDMA optical outgassing oxide particles penetration performed PET film plasma plume polyethylene polyimide polymer projectile properties Protection of Materials protons quartz glass reaction reflectance roll thrusters sail material sample sheet resistivity shown in figure shows silicone simulation solar array solar cells Space Environment spacecraft spectral spectrum Structures from Space substrate surface temperature tensile thermochromic thermocycling thickness transmittance vacuum ultraviolet VUV exposure VUV suns water dump wavelength