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NASA CSTI Earth-to-orbit propulsion R/T program overviewThe topics presented are covered in viewgraph form. The programmatic objectives are to develop and validate technology, design tools, and methodologies needed for the development of a new generation of lower cost, operationally-efficient, long-life, highly reliable ETO propulsion systems. The technical objectives are: (1) high quality, low cost, inspectable manufacturing; (2) safe shutdown to fault tolerance operations for safety; (3) condition monitoring diagnostics for maintainability; (4) automatic servicing and checkout for ground operations; (5) max commensurate with life for performance; and full flow, combined cycle for advanced cycles.
Document ID
19930074433
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Moses, James L.
(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 8 p (SEE N93-71873 13-81)
Subject Category
Administration And Management
Report/Patent Number
PR7
Accession Number
93N71880
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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