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There are a total of 7 record(s) matching your query.
Sorted by: Date Added To NTRS in Descending order
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Metal Matrix Composite LOX Turbopump Housing Via Novel Tool-Less Net-Shape Pressure Infiltration Casting Technology
Author(s): Shah, Sandeep; Lee, Jonathan; Bhat, Biliyar; Wells, Doug; Gregg, Wayne; Marsh, Matthew; Genge, Gary; Forbes, John; Salvi, Alex; Cornie, James A., et al.
Abstract: This presentation provides an overview of the effort by Metal Matrix Cast Composites, Inc. to redesign turbopump housing joints using metal matrix composite material and a toolless net-shape pressure infiltration casting ...
NASA Center: Marshall Space Flight Center Publication Year: 2002
Added to NTRS: 2008-06-02
Document ID: 20020094390
Metal Matrix Composite LOX Turbopump Housing via Novel Tool-less Net-Shape Pressure Infiltration Casting Technology
Author(s): Shah, Sandeep; Lee, Jonathan; Bhat, Biliyar; Wells, Doug; Gregg, Wayne; Marsh, Matthew; Genge, Gary; Forbes, John; Salvi, Alex; Cornie, James A., et al.
Abstract: Metal matrix composites for propulsion components offer high performance and affordability, resulting in low weight and cost. The following sections in this viewgraph presentation describe the pressure infiltration casting ...
NASA Center: Marshall Space Flight Center Publication Year: 2003
Added to NTRS: 2005-11-24
Document ID: 20040083976
Thermo-Mechanical Turbopump Design and Analysis Tools
Author(s): Platt, Michael J.; Cook, Conan; Marsh, Matthew
Abstract: The design and analysis tools developed in this project improve the turbopump design process through data synthesis of component models, encompassing information from pump and turbine designs, in addition to shafts, ...
NASA Center: Marshall Space Flight Center Publication Year: 2002
Added to NTRS: 2005-10-10
Document ID: 20020073798
Flow Simulation in Secondary Flow Passages of a Rocket Engine Turbopump
Author(s): Schallhorn, Paul; Majumdar, Alok; VanHooser, Katherine; Marsh, Matthew
Abstract: This paper presents application of a Generalized Fluid System Simulation Program (GFSSP) to model fluid flow in a very complex secondary flow circuit of a rocket engine turbopump, SIMPLEX. SIMPLEX was a low cost turbopump ...
NASA Center: Marshall Space Flight Center Publication Year: 1998
Added to NTRS: 2005-08-25
Document ID: 19980197470; Report Number: NAS 1.26:207925, NASA/CR-1998-207925
Metal Matrix Composite LOX Turbopump Housing Via Novel Tool-Less Net-Shape Pressure Infiltration Casting Technology
Author(s): Shah, Sandeep; Lee, Jonathan; Bhat, Biliyar; Wells, Doug; Gregg, Wayne; Marsh, Matthew; Genge, Gary; Forbes, John; Salvi, Alex; Cornie, James A., et al.
Abstract: Metal matrix composites (MMC) offer relatively higher specific strength, specific stiffness, lower coefficient of thermal expansion (CTE) and lower density as compared with conventional alloys. These unique properties make ...
NASA Center: Marshall Space Flight Center Publication Year: 2001
Added to NTRS: 2004-11-03
Document ID: 20010037927
Metal Matrix Composite LOX Turbopump Housing Via Novel Tool-Less Net-Shape Pressure Infiltration Casting Technology
Author(s): Shah, Sandeep; Lee, Jonathan; Bhat, Biliyar; Wells, Doug; Gregg, Wayne; Marsh, Matthew; Genge, Gary; Forbes, John; Salvi, Alex; Cornie, James A.; Sung, Michael; Zhang, Shi-Yu
Abstract: Metal matrix composites (MMC) offer relatively higher specific strength, specific stiffness, lower coefficient of thermal expansion (CTE) and lower density as compared with conventional alloys. These unique properties make ...
NASA Center: Marshall Space Flight Center Publication Year: 2001
Added to NTRS: 2004-11-03
Document ID: 20010021180
Metal Matrix Composite LOX Turbopump Housing Via Novel Tool-less Net-Shape Pressure Infiltration Casting Technology
Author(s): Shah, Sandeep; Lee, Jonathan; Bhat, Biliyar; Wells, Doug; Gregg, Wayne; Marsh, Matthew; Genge, Gary; Forbes, John; Salvi, Alex; Cornie, James A., et al.
Abstract: Metal matrix composites (MMC) offer relatively higher specific strength, specific stiffness, lower coefficient of thermal expansion (CTE) and lower density as compared with conventional alloys. These unique properties make ...
NASA Center: Marshall Space Flight Center Publication Year: 2002
Added to NTRS: 2004-11-03
Document ID: 20030001002
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