NASA NTRS · 19870013339
Progress on thin-film sensors for space propulsion technology
Abstract
The 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.
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Kim, Walter S.. 1987-01-01. Progress on thin-film sensors for space propulsion technology. https://ntrs.nasa.gov/citations/19870013339
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