全部 标题 作者
关键词 摘要

OALib Journal期刊
ISSN: 2333-9721
费用:99美元

查看量下载量

相关文章

更多...

Optical Response of Metakaolin after Ultraviolet and High Energy Electron Exposure

DOI: 10.1155/2014/623832

Full-Text   Cite this paper   Add to My Lib

Abstract:

Metakaolin, which is part of a class of inorganic polymers called geopolymers, is being tested currently for its use as a lightweight mirror material in spacecraft applications. Metakaolin, as with most geopolymers, has the advantages of low initial coefficient of thermal expansion, easy preparation at room temperature and pressure, and high specific strength. Even though metakaolin has been known as a structural material for millennia, it has not been properly vetted for use as a material in spacecraft applications, especially with respect to exposure to its environments. This research highlights one particular aspect of response to the space environment; that is, how do the optical properties of metakaolin change after subjugation to bombardment by ultraviolet and high energy electron radiation? These two radiation sources are common in low earth orbit and a primary cause of degradation of organic polymers in space. Photospectroscopic analysis showed that ultraviolet in combination with high energy electrons causes changes in the metakaolin which need to be accounted for due to their potential impacts on the thermal management of a spacecraft and during application in composite mirror structures. 1. Introduction The primary choice of mirror material for spacecraft imaging optics, since the beginning of the space age, has been monolithic glass. Monolithic glass mirrors have enabled spacecraft designers to achieve mirror diameters of over 1?m, and they are well understood in terms of mechanical and thermal performance as monolithic glass variants have been one of the first man-made construction materials [1]. However, material performance requirements for the future space mirrors for advanced imaging missions necessitate a lower areal density than glass with similar if not superior mechanical strength. Additionally, any material chosen must also be able to withstand the unique environment of low earth orbit, namely the near-vacuum conditions, radiation environment and interaction with atomic oxygen. The space environment poses unique hazards for materials. There is a specific concern with any material, including geopolymers, and it is about the behavior under the radiation environment encountered in orbit. Previous investigations, both on the ground and in-flight experiments, have shown that significant degradation of the organic polymer strength occurs due to the increased cross-linking of polymer networks after absorbing the radiation emitted from the sun or deep space. The typical radiation environment includes exposure to ultraviolet and gamma

References

[1]  P. S. Carlin, “Lightweight mirror systems for spacecraft—an overview of materials & manufacturing needs,” in Proceedings of the IEEE Aerospace Conference, pp. 169–181, Big Sky, Mont, USA, March 2000.
[2]  R. A. Dressler, Chemical Dynamics in Extreme Environments, World Scientific, Singapore, 2001.
[3]  J. Haffke and J. Woolam, “Synergistic degredation of CV-1144-O due to ultraviolet radiation and heat,” in Proceedings of the 6th annual International Conference on Protection of Materials and Structures from Space Environment (ICPMSE '02), pp. 183–191, Toronto, Canada, May 2002.
[4]  L. E. Matson, M. Y. Chen, B. deBlonk, and I. Palusinski, “Silicon carbide technologies for lightweighted aerospace mirrors,” in Proceedings of the Advanced Maui Optical and Space Surveillance Technologies Conference (AMOSTech '08), Maui, Hawaii, USA, September 2008.
[5]  P. N. Balaguru and M. Arafa, “Geopolymer coating demonstration project for route I-295 scenic overlook,” New Jersey Department of Transportation Document FHWA-NJ-2005-021, 2006.
[6]  M. Bellotto, A. Gualtieri, G. Artioli, and S. M. Clark, “Kinetic study of the kaolinite-mullite reaction sequence. Part I: kaolinite dehydroxylation,” Physics and Chemistry of Minerals, vol. 22, no. 4, pp. 207–217, 1995.
[7]  American Society for Testing and Materials, “E 512-94 (Reapproved 2004) Standard practice for combined, simulated space environment testing of thermal control materials with electromagnetic and particulate radiation,” ASTM International Document E512-94, 2004.
[8]  C. A. Cerbus and P. S. Carlin, “SCEPTRE: the air force combined space environment facility,” in Proceedings of the 1st Spacecraft Thermal Control Symposium Proceedings, STCS-94USAF Phillips Laboratory, Albuquerque, NM, USA, 1994.
[9]  J. Frercks, H. Weber, and G. Wiesenfeldt, “Reception and discovery: the nature of Johann Wilhelm Ritter's invisible rays,” Studies in History and Philosophy of Science Part A, vol. 40, no. 2, pp. 143–156, 2009.

Full-Text

Contact Us

service@oalib.com

QQ:3279437679

WhatsApp +8615387084133