NASA NTRS · 19850018551
Advanced High Pressure O2/H2 Technology
Abstract
Activities 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.
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Morea, S. F., Wu, S. T.. 1985-04-01. Advanced High Pressure O2/H2 Technology. https://ntrs.nasa.gov/citations/19850018551
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