NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
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
20040182396
Document Type
Conference Proceedings
Authors
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
NASA/CP-2004-212963/VOL1
E-14436-1/VOL1
Meeting Information
2003 NASA Seal/Secondary Air System Workshop(Cleveland, OH)
Funding Number(s)
WBS: WBS 22-708-48-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

NameType 20040182396.pdf STI

Related Records

IDRelationTitle20040182412Analytic SubsidiaryOverview of NASA Glenn Seal Developments20040182400Analytic SubsidiaryNASA Ultra Efficient Engine Technology Project Overview20040182402Analytic SubsidiaryNon-Contacting Finger Seal Developments and Design Considerations20040182410Analytic SubsidiaryHigh Temperature Propulsion System Structural Seals for Future Space Launch Vehicles20040182414Analytic SubsidiaryInvestigations of High Pressure Acoustic Waves in Resonators with Seal-Like Features20040182401Analytic SubsidiaryLow Emissions Alternative Power (LEAP)20040182398Analytic SubsidiaryCompliant Foil Seal Investigations20040182408Analytic SubsidiaryAdvanced Control Surface Seal Development for Future Space Vehicles20040182411Analytic SubsidiaryControls Considerations for Turbine Active Clearance Control20040182404Analytic SubsidiaryNumerical Investigations of High Pressure Acoustic Waves in Resonators20040182413Analytic SubsidiaryTest Rig for Evaluating Active Turbine Blade Tip Clearance Control Concepts20040182399Analytic Subsidiary"Bimodal" Nuclear Thermal Rocket (BNTR) Propulsion for Future Human Mars Exploration Missions