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An Overview of High Temperature Seal Development and Testing Capabilities at the NASA Glenn Research CenterThe 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


Document ID
20150000141
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Demange, Jeffrey J.
(Toledo Univ. Toledo, OH, United States)
Taylor, Shawn C.
(Toledo Univ. Toledo, OH, United States)
Dunlap, Patrick H.
(NASA Glenn Research Center Cleveland, OH, United States)
Steinetz, Bruce M.
(NASA Glenn Research Center Cleveland, OH, United States)
Finkbeiner, Joshua R.
(NASA Glenn Research Center Cleveland, OH, United States)
Proctor, Margaret P.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
January 5, 2015
Publication Date
July 28, 2014
Subject Category
Spacecraft Design, Testing And Performance
Structural Mechanics
Report/Patent Number
GRC-E-DAA-TN16339
Meeting Information
Meeting: AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Location: Cleveland, OH
Country: United States
Start Date: July 28, 2014
End Date: July 30, 2014
Sponsors: American Society for Engineering Education, American Inst. of Aeronautics and Astronautics, American Society of Mechanical Engineers, Society of Automotive Engineers, Inc.
Funding Number(s)
CONTRACT_GRANT: NNC08CA35C
CONTRACT_GRANT: NNC13BA10B
WBS: WBS 747797.06.13.07.30.03
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
National Aerospace Plane
thermal seals
thermal barriers
space shuttles
thermal protection
compression tests
low temperature
high temperature
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