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Earth-to-orbit propulsion turbomachinery subsystem: OverviewThe topics presented are covered in viewgraph form. The objectives are: (1) to develop the technology related to the turbomachinery systems of high performance rocket engines, which focuses on advanced design methodologies and concepts, develops high performance turbomachinery data bases, and validates turbomachinery design tools; and (2) specific turbomachinery subsystems and disciplines, which focus on turbine stages, pump stages, bearings, deals, structural dynamics, complex flow paths, materials, manufacturability, producibility, and inspectability, rotordynamics, and fatigue/fracture/life.
Document ID
19930074435
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Schutzenhofer, L. A. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Garcia, R. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1991
Publication Information
Publication: NASA, Washington, SSTAC(ARTS Review of the Draft Integrated Technology Plan (ITP). Volume 2: Propulsion Systems 22 p (SEE N93-71873 13-81)
Subject Category
Administration And Management
Report/Patent Number
PR9
Accession Number
93N71882
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19930074426Collected WorksSSTAC/ARTS Review of the Draft Integrated Technology Plan (ITP). Volume 2: Propulsion Systems
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