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The Development of a PdCr Integral Weldable Strain Measurement System Based on NASA Lewis PdCr/Pt Strain Sensor for User-Friendly Elevated Temperature Strain MeasurementsThis report describes the development of a user friendly weldable strain gage employing the NASA Lewis PdCr/Pt wire strain sensor. The NASA sensors are pre-attached to Hastelloy X or Titanium alloy shims using name spray techniques developed under previous NASA programs. The weldable sensors are then pre-stabilized for 50 hours at 780 C in air. A weldable terminal and high temperature cable is then connected to the sensor and the assembly is pre-calibrated over the full test temperature range. Calibrated resistors are inserted into a bridge completion module at the cool end of the cable to condition the sensor in half or full bridge configuration. The sensor is attached to the structure using a common capacitive discharge spot welder. No additional high temperature stabilization or calibration is required. The resultant device is a pre-calibrated strain transducer which can be plugged into any common variety strain instrumentation.
Document ID
19970012640
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wnuk, S. P., Jr.
(HITEC Products, Inc. Ayer, MA United States)
Wnuk, V. P.
(HITEC Products, Inc. Ayer, MA United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1997
Subject Category
Spacecraft Instrumentation
Report/Patent Number
NASA-CR-202316
E-10617
NAS 1.26:202316
Report Number: NASA-CR-202316
Report Number: E-10617
Report Number: NAS 1.26:202316
Accession Number
97N16892
Funding Number(s)
PROJECT: RTOP 523-21-13
CONTRACT_GRANT: NASA Order C-86401-D
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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