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The Calibrations of Space Shuttle Main Engines High Pressure TransducersPreviously, high pressure transducers that were used on the Space Shuttles Main Engine (SSME) exhibited a severe drift after being tested on the SSME. The Experimental Testing Technology Division (ETTD) designed some new transducers that would not exhibit a severe drift over a short period of time. These transducers were calibrated at the Test Bed at Marshall Space Flight Center (MSFC). After the high pressure transducers were calibrated, the transducers were placed on the SSME and fired. The transducers were then sent to the NASA LaRC to be recalibrated. The main objectives of the recalibrations was to make sure that the transducers possessed the same qualities as they did before they were fired on the SSME. Other objectives of the project were to determine the stability of the transducers and to determine whether the transducers exhibited a severe drift.
Document ID
19970003116
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Steward, Christopher S.
(Norfolk State Univ. VA United States)
Date Acquired
August 17, 2013
Publication Date
January 1, 1995
Publication Information
Publication: Langley Aerospace Research Summer Scholars
Volume: Part 2
Subject Category
Spacecraft Propulsion And Power
Accession Number
97N11881
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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