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タイトルAn Overview of High Temperature Seal Development and Testing Capabilities at the NASA Glenn Research Center
本文(外部サイト)http://hdl.handle.net/2060/20150000141
著者(英)Demange, Jeffrey J.; Steinetz, Bruce M.; Proctor, Margaret P.; Taylor, Shawn C.; Dunlap, Patrick H.; Finkbeiner, Joshua R.
著者所属(英)NASA Glenn Research Center
発行日2014-07-28
言語eng
内容記述The NASA Glenn Research Center (GRC), partnering with the University of Toledo, has a long history of developing and testing seal technologies for high-temperature applications. The GRC Seals Team has conducted research and development on high-temperature seal technologies for applications including advanced propulsion systems, thermal protection systems (airframe and control surface thermal seals), high-temperature preloading technologies, and other extreme-environment seal applications. The team has supported several high-profile projects over the past 30 years and has partnered with numerous organizations, including other government entities, academic institutions, and private organizations. Some of these projects have included the National Aerospace Space Plane (NASP), Space Shuttle Space Transport System (STS), the Multi-Purpose Crew Vehicle (MPCV), and the Dream Chaser Space Transportation System, as well as several high-speed vehicle programs for other government organizations. As part of the support for these programs, NASA GRC has developed unique seal-specific test facilities that permit evaluations and screening exercises in relevant environments. The team has also embarked on developing high-temperature preloaders to help maintain seal functionality in extreme environments. This paper highlights several propulsion-related projects that the NASA GRC Seals Team has supported over the past several years and will provide an overview of existing testing capabilities
NASA分類Spacecraft Design, Testing and Performance; Structural Mechanics
レポートNOGRC-E-DAA-TN16339
権利Copyright, Distribution as joint owner in the copyright
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/61884


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