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Advanced High Pressure O2/H2 TechnologyActivities in the development of advanced high pressure oxygen-hydrogen stage combustion rocket engines are reported. Particular emphasis is given to the Space Shuttle main engine. The areas of engine technology discussed include fracture and fatigue in engine components, manufacturing and producibility engineering, materials, bearing technology, structure dynamics, fluid dynamics, and instrumentation technology.
Document ID
19850018551
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Morea, S. F. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Wu, S. T. (Alabama Univ. Huntsville, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1985
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CP-2372
NAS 1.55:2372
Accession Number
85N26862
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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