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Material technologyAdvanced high pressure O2/H2 propulsion systems as exemplified by the Space Shuttle Main Engine (SSME) create challenging operating environments for materials. Many components operate in either hydrogen or hydrogen-steam environments which may significantly degrade the performance of common alloys. The objective of the materials technology projects is to develop and evaluate candidate materials for application in advanced high pressure O2/H2 propulsion systems. These new and improved materials are to improve the durability or performance of the SSME or derivative engine. The program includes projects on the following topics: (1) Hydrogen Resistant Alloys; (2) High Pressure O2 Ignition and Burning; (3) Improved Turbine Blades; (4) Improved Turbine Disk Material; (5) Impact Reactivity in High Pressure O2; and Fiber Reinforced Superalloys.
Document ID
19850018559
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dreshfield, R. L.
(NASA Lewis Research Center Huntsville, AL, United States)
Mcpherson, W. B.
(NASA Marshall Space Flight Center)
Date Acquired
August 12, 2013
Publication Date
April 1, 1985
Publication Information
Publication: Advan. High Pressure O2(H2 Technol.
Subject Category
Chemistry And Materials (General)
Accession Number
85N26870
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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