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Seal Technology for Hypersonic Vehicle and Propulsion: An OverviewHypersonic vehicles and propulsion systems pose an extraordinary challenge for structures and materials. Airframes and engines require lightweight, high-temperature materials and structural configurations that can withstand the extreme environment of hypersonic flight. Some of the challenges posed include very high temperatures, heating of the whole vehicle, steady-state and transient localized heating from shock waves, high aerodynamic loads, high fluctuating pressure loads, potential for severe flutter, vibration, and acoustic loads and erosion. Correspondingly high temperature seals are required to meet these aggressive requirements. This presentation reviews relevant seal technology for both heritage (e.g. Space Shuttle, X-15, and X-38) vehicles and presents several seal case studies aimed at providing lessons learned for future hypersonic vehicle seal development. This presentation also reviews seal technology developed for the National Aerospace Plane propulsion systems and presents several seal case studies aimed at providing lessons learned for future hypersonic propulsion seal development.
Document ID
20080047343
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Steinetz, Bruce M.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 24, 2013
Publication Date
February 26, 2008
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
E-16776
Report Number: E-16776
Meeting Information
Meeting: Short Course on Hypersonics Structures and Materials
Location: Hampton, VA
Country: United States
Start Date: February 26, 2008
End Date: February 28, 2008
Sponsors: National Institute of Aerospace
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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