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Progress on thin-film sensors for space propulsion technologyThe objective is to develop thin-film thermocouples for Space Shuttle Main Engine (SSME) components. Thin-film thermocouples have been developed for aircraft gas turbine engines and are in use for temperature measurement on turbine blades to 1800 F. The technology established for aircraft gas turbine engines will be adapted to the materials and environment encountered in the SSME. Specific goals are to expand the existing in-house thin-film sensor technology and to test the survivability and durability of thin-film sensors in the SSME environment.
Document ID
19870013339
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kim, Walter S. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1987
Publication Information
Publication: Structural Integrity and Durability of Reusable Space Propulsion Systems
Subject Category
Instrumentation And Photography
Accession Number
87N22772
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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