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Teledyne Taber 206-1000 and 2210-3000 pressure transducer proof test and burst testThe range accuracy and structural integrity of the Teledyne Taber 206-1000 and 2210-3000 pressure transducers are verified and multiple uses are studied to determine is they have a significant effect on the transducers. Burst pressure for these transducers was also established. The Teledyne Taber 206-1000 pressure transducer is used to measure chamber pressure on full-scale space shuttle rocket motors. The Teledyne Taber 2210-3000 pressure transducer is used to measure igniter pressure. The Teledyne Taber transducer has very good temperature stability and was used on all full-scale solid rocket motors, so there is a large data base established using this transducer.
Document ID
19890015223
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ricks, G. A.
(Morton Thiokol Brigham City, UT, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1989
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-CR-183672
NAS 1.26:183672
ECS-SS-2801
MTI-PUBL-89734
WBS-HQ302-10-10
TWR-19248
Report Number: NASA-CR-183672
Report Number: NAS 1.26:183672
Report Number: ECS-SS-2801
Report Number: MTI-PUBL-89734
Report Number: WBS-HQ302-10-10
Report Number: TWR-19248
Accession Number
89N24594
Funding Number(s)
CONTRACT_GRANT: NAS8-30490
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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