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2003 NASA Seal/Secondary Air System WorkshopThe following reports were included in the 2003 NASA Seal/Secondary Air System Workshop:Low Emissions Alternative Power (LEAP); Overview of NASA Glenn Seal Developments; NASA Ultra Efficient Engine Technology Project Overview; Development of Higher Temperature Abradable Seals for Industrial Gas Turbines; High Misalignment Carbon Seals for the Fan Drive Gear System Technologies; Compliant Foil Seal Investigations; Test Rig for Evaluating Active Turbine Blade Tip Clearance Control Concepts; Controls Considerations for Turbine Active Clearance Control; Non-Contacting Finger Seal Developments and Design Considerations; Effect of Flow-Induced Radial Load on Brush Seal/Rotor Contact Mechanics; Seal Developments at Flowserve Corporation; Investigations of High Pressure Acoustic Waves in Resonators With Seal-Like Features; Numerical Investigations of High Pressure Acoustic Waves in Resonators; Feltmetal Seal Material Through-Flow; "Bimodal" Nuclear Thermal Rocket (BNTR) Propulsion for Future Human Mars Exploration Missions; High Temperature Propulsion System Structural Seals for Future Space Launch Vehicles; Advanced Control Surface Seal Development for Future Space Vehicles; High Temperature Metallic Seal Development for Aero Propulsion and Gas Turbine Applications; and BrazeFoil Honeycomb.
Document ID
Acquisition Source
Glenn Research Center
Document Type
Conference Proceedings
Steinetz, Bruce M.
(NASA Glenn Research Center Cleveland, OH, United States)
Hendricks, Robert C.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
September 1, 2004
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
Meeting Information
Meeting: 2003 NASA Seal/Secondary Air System Workshop
Location: Cleveland, OH
Country: United States
Start Date: November 5, 2003
End Date: November 6, 2003
Sponsors: NASA Glenn Research Center
Funding Number(s)
WBS: WBS 22-708-48-01
Distribution Limits
Work of the US Gov. Public Use Permitted.
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